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for tests of the LK Lunar lander in low Earth | orbit, as part of the Soviet lunar programme. |
arth asteroid, which basically shares the same | orbit as Earth itself around the sun, is a very dang |
ule engine to raise the spacecraft into a high | orbit, as had been done in Apollo 4, in order to com |
Soviet Union launches the Voskhod 1 into Earth | orbit as the first spacecraft with a multi-person cr |
he orbital plane is a defining parameter of an | orbit; as in general, it will take a very large amou |
d the satellite into a geosynchronous transfer | orbit, as had originally been planned. |
s engines) that must be carried all the way to | orbit, as opposed to oxidizer mass that would be bur |
celestial body has been discovered in the same | orbit as Earth. |
The ATDA in | orbit as seen from Gemini 9A. |
anymede, by contrast, is not in a heliocentric | orbit as it orbits Jupiter. |
COSPAR ID: 1960-ETA 2 or 1960-007B(still in | orbit as of March 2007) |
th its apogee and its perigee to geostationary | orbit as well as to decrease the orbital inclination |
ed to go past the Moon and into a heliocentric | orbit as planned, but did reach an altitude of 102,3 |
sses close to the Sun on its highly elliptical | orbit; as the comet warms, parts of it sublimate. |
lan to draw two outlying planets into the same | orbit as Juconda. |
ed position over the years due to their mutual | orbit as binary stars. |
-orbit testing, it was placed in geostationary | orbit at 10° East, from where it provided broadcast |
eansat-2 and three further CubeSats in a polar | orbit at 730 km altitude. |
s 524 was successfully launched into low Earth | orbit at 13:19:58 GMT on 11 October 1972. |
ime that two female mission commanders were in | orbit at the same time. |
o have operated in a Sun-synchronous low Earth | orbit, at an altitude of 480 kilometres (300 mi) and |
ing launch, it was positioned in geostationary | orbit at a longitude of 90° West for on-orbit testin |
It was launched into a geosynchronous | orbit at 22:43 GMT on 18 August 2008, by a Proton-M/ |
It was meant to circle the Earth on a circular | orbit at 750 km altitude, inclined 17.5 ° from the E |
o the star HD 109749, taking only 5.24 days to | orbit at the distance of 0.063 AU. |
e fixing submanifold may not intersect a gauge | orbit at all or it may intersect it more than once. |
It takes only 4.188 days (or 100.5 hours) to | orbit at an orbital distance of 7.6 gigameters (0.05 |
-orbit testing, it was placed in geostationary | orbit at 123° East, from where it provides communica |
ur I rocket and successfully entered low Earth | orbit at approximately 285 miles above the Earth, it |
orbit testing, it was placed in geosynchronous | orbit at 145° East, from where it provides communica |
aunch, GOES 11 was positioned in geostationary | orbit at a longitude of 104° West for testing and on |
-orbit testing, it was placed in geostationary | orbit at 30° West, from where it provides communicat |
This planet takes about 499 days to | orbit at an orbital distance about 1.28 AU and range |
By comparison, geostationary satellites | orbit at 5.6 Earth radii and GPS satellites orbit at |
is an extrasolar planet that takes 198 days to | orbit at the distance of 0.78 AU. |
Lewis was to have raised itself into a higher | orbit, at an altitude of 523 kilometres (325 mi). |
s 558 was successfully launched into low Earth | orbit at 13:19:58 GMT on 17 May 1973. |
is intended to be positioned in geostationary | orbit at a longitude of 113º East, where it will rep |
gnitude orange dwarf that takes 26.28 years to | orbit at 10.3 AU around the primary in an elliptical |
It was found to have a retrograde | orbit, at a very high angle of inclination to the pl |
r 6.06 μpc from the star, taking 1.25 years to | orbit at 29.9 km/s around the star. |
of 2003 into a sun-synchronous 830 km circular | orbit at a local time of 0800-2000 UT. |
-orbit testing, it was placed in geostationary | orbit at 162° East, from where it provides communica |
-orbit testing, it was placed in geostationary | orbit at 123° West, from where it provided communica |
on July 17, 1991 into a Sun-synchronous polar | orbit at a height of 782-785 km. |
e to the parent star, taking only 3.92 days to | orbit at the average distance of 7.9 gigameters. |
It takes only 4.125 days (or 99 hours) to | orbit at a distance of 8.3 gigameters (0.0555 AU) aw |
led the presence of a long-period planet in an | orbit at around 5 AU from the star. |
Florida carrying the Skylab space station into | orbit, at 17:30 GMT, on May 14, 1973. |
s 611 was successfully launched into low Earth | orbit at 09:29:58 GMT on 28 November 1973. |
ngine would carry the spacecraft to a circular | orbit at an altitude of about 25,000 miles around th |
It is positioned in geostationary | orbit at a longitude of 70 degrees East. |
na 15 - an unmanned Soviet spacecraft in lunar | orbit at the time, began its descent to the lunar su |
It is positioned in geostationary | orbit at a longitude of 119° West, from where it is |
The article says "...parking | orbit at 185 km altitude 0 minutes after launch." |
MJ planet taking 33.15 Ms to | orbit at 154.1 Gm or 4.99 μpc from the star at 36% e |
It will replace AMOS-1 in geosynchronous | orbit at 4°W. |
Its NORAD ID is 17527; it is in a polar | orbit at roughly 900km altitude, but has not been ac |
The satellite is to fly in a 400 km high polar | orbit at an inclination of 97 degrees. |
tal period is approximately 570 days, and they | orbit at a distance of approximately 4000 km (closes |
ed to be the source of long-period comets that | orbit at thousands of times Pluto's distance from th |
was tested against a US Air Force satellite in | orbit at a distance of 432 km (268 mi). |
from its primary star, as compared to Earth's | orbit at approximately one astronomical unit away fr |
rocket placed the craft into a nearly circular | orbit at an altitude of 697 kilometres (433 mi) and |
Unlike comets, which spend most of their | orbit at Jupiter-like or greater distances from the |
was extended after Odyssey entered the mapping | orbit at Mars. |
orbit testing, it was placed in geosynchronous | orbit at 11° West, from where it provides communicat |
This planet orbits in an eccentric | orbit at 1.76 AU from its star (HD 128311). |
s, the variation of the Moon in its elliptical | orbit at each event causes the actual eclipse time t |
This star takes 2117 days or 5.797 years to | orbit at the average distance of 3.27 Astronomical U |
s 498 was successfully launched into low Earth | orbit at 09:29:58 GMT on 5 July 1972. |
es of weather patterns from an almost circular | orbit, at an altitude ranging from 435.5 miles (700. |
s 608 was successfully launched into low Earth | orbit at 12:29:58 GMT on 20 November 1973. |
s 545 was successfully launched into low Earth | orbit at 11:44:50 GMT on 24 January 1973. |
lly reached an inclined (13.1°) geosynchronous | orbit at 34.8°East. |
Arabsat 1B was placed into a geosynchronous | orbit at a longitude of 26° East. |
-orbit testing, it was placed in geostationary | orbit at 73° East, from where it provides broadcast |
However the satellite failed to | orbit at any stage. |
It was intended to operate in a circular | orbit at an altitude of around 1,000 kilometres (620 |
entire planet whilst circling Earth in a polar | orbit at 514 km altitude. |
s 487 was successfully launched into low Earth | orbit at 11:59:59 GMT on 21 April 1972. |
TDRS-G will reside in geosynchronous | orbit at 22,300 miles (35,888 kilometers) at 178 deg |
It is positioned in Geostationary | orbit at a longitude of 110° West, from where it is |
ts (such as asteroids, moons, or planets) that | orbit at the same (or very similar) distance from th |
e spacecraft is intended for a sun-synchronous | orbit at an altitude of 684 km (425 mi) and an incli |
RVIS-2 operates in a Sun-synchronous low Earth | orbit, at an altitude of 1,200 kilometres (750 mi) a |
carrier rocket, into a Geosynchronous transfer | orbit at 09:23, launched by an H-IIA carrier rocket |
s 580 was successfully launched into low Earth | orbit at 11:24:55 GMT on 22 August 1973. |
It will be operated in geosynchronous | orbit, at a longitude of 7º West. |
s 553 was successfully launched into low Earth | orbit at 11:49:55 GMT on 12 April 1973. |
o reach 2.94 km/s at infinity from a low Earth | orbit at, say 200 km altitude, requires a 3.61 km/s |
ment Shuttle performance during launch, boost, | orbit, atmospheric entry and landing phases. |
Beyond | Orbit Azonal Runabout |
The eccentric | orbit became clear with the discovery of the brown d |
less than 300 days that orbits in an eccentric | orbit, because the parent star is 65% more massive t |
rly during its first try on the mission's 37th | orbit, because the orbiter was not at the correct at |
weight to be sent to the surface and back into | orbit, because the fuel needed to travel to and from |
They maintain | orbit because of the force of gravity between them. |
ied the S-55 satellite, but this did not reach | orbit because the third stage failed to ignite. |
In this limit, the equation for the | orbit becomes |
months studying the planet and its moons from | orbit, before landing on Phobos. |
e best and most accurate modeling for the Moon | orbit before the availability of digital computers w |
n flaw it failed within three days of reaching | orbit, before it became operational. |
fly to put the spacecraft into a parking Earth | orbit, before restarting the engine for flight to th |
put from the pilot, and as he began his second | orbit began testing a yaw manoeuvre using the Earth |
ates the Oblivion planet that's taken up Earth | orbit behind the Moon and also investigates the land |
American mathematician who discovered a stable | orbit between the Earth and the Moon, called an Aren |
ve been the perturbations brought about in its | orbit, between successive appearances, by the action |
he Einstein Observatory (HEAO 2) satellite, in | orbit between November 1978 and April 1981. |
The satellites | orbit between 833 or 870 kilometers (+/- 19 kilomete |
of the debris is 110°K, which places it in an | orbit between 4 and 6 AU from the star, or about the |
In 1998 the company established | Orbit Bexley Housing Association to take on the mana |
In October 2007 | Orbit Bexley and Thanet Community were merged to for |
See, the thing is that planets can | orbit black holes, yes, but given the fact that enti |
Publisher | Orbit Books released the book's cover on February 1, |
2010, USA, | Orbit Books ISBN 0-316-07415-2, Pub date 1 September |
2011, UK, | Orbit Books ISBN 0-356-50009-8, Pub date 7 July 2011 |
2011, USA, | Orbit Books ISBN 0-316-12719-1, Pub date 28 June 201 |
2010, UK, | Orbit Books ISBN 1-841-49972-2, Pub date 2 September |
see also | Orbit Books for the UK Book publisher |
Orbit Books purchased the series for UK publication, | |
In November 2007, | Orbit Books announced that they had purchased the ri |
London: | Orbit Books, 2009 (paperback). |
Yen Press, like series publisher | Orbit Books, is a division of Hachette Book Group. |
First published in September 2010 by | Orbit Books, Blameless is the third book in a projec |
Scheduled to be published on June 28, 2011, by | Orbit Books, Heartless is the fourth book in the New |
Mayhar also owned and operated The View From | Orbit Bookstore in Nacogdoches, Texas with her husba |
because it nearly represents a single-stage to | orbit booster, but is actually a stage and a half bo |
Its | orbit brings it further away from the galactic cente |
candinavian Skin Trade" was remixed by William | Orbit but never released. |
ng up to 100 tonnes of mass to a geostationary | orbit, but was never flown. |
L-6/A-2-e launcher successfully achieved Earth | orbit, but the spacecraft failed to escape orbit for |
which did launch the oldest satellite still in | orbit, but they did utilize his ionization process a |
This time, the player was not confined to | orbit but could land on and explore or mine planets. |
n appreciable tidal effect on the planets they | orbit, but several moons in the solar system are und |
After 375 seconds, it went outside of Earth | orbit, but it went out disastrously. |
rcury, by some called Apollo; it has a similar | orbit, but is by no means similar in magnitude or po |
s around the L4 point of Mars in a very stable | orbit, but little is known about its shape so the Ya |
the South Pole in an attempt to achieve polar | orbit, but was unsuccessful. |
Johann Franz Encke attempted to calculate the | orbit but was left with very large errors. |
, 7 hours and 43.2 minutes to go around in its | orbit; but since the Earth-Moon system advances arou |
load scientific instrument launched into Earth | orbit by NASA in 1999 on board the Terra (EOS AM) Sa |
after launch, and was raised to geostationary | orbit by means of an Inertial Upper Stage. |
a Center catalogued 172 spacecraft placed into | orbit by launches which occurred in 1967. |
after launch, and was raised to geostationary | orbit by means of an Inertial Upper Stage. |
As the second module sent into | orbit by the company, this spacecraft builds on the |
for its age and so is possibly pulled into its | orbit by another planet. |
en found on Mars in infrared images taken from | orbit by Mars Odyssey's thermal imager. |
They are joined, immediately beneath the | orbit, by filaments from the facial nerve, forming w |
It was successfully placed into | orbit by International Launch Services, who also lau |
very, and boosted to a geosynchronous transfer | orbit by means of a PAM-D upper stage. |
Simulations of its | orbit by scientists of the Deep Space 1 project pred |
intended to have been launched into low Earth | orbit by the Soyuz 11A511 carrier rocket. |
after launch, and was raised to geosynchronous | orbit by means of an Inertial Upper Stage. |
its launch it raised itself into geostationary | orbit by means of its onboard R-4D apogee motor, and |
ction satellites were lifted to geosynchronous | orbit by a fourth stage of a new, experimental desig |
After its launch into Geo-synchronous transfer | orbit by Soyuz, AMOS-2 was taken to its final geo-st |
board the Terra satellite launched into Earth | orbit by NASA in 1999. |
s later successfully transferred to its proper | orbit by the Inertial Upper Stage booster. |
It will raise itself into geostationary | orbit by means of its onboard R-4D apogee motor. |
intended to have been launched into low Earth | orbit by the Soyuz 11A511 carrier rocket. |
Galileo was launched into | orbit by the Space Shuttle Atlantis mission STS-34 o |
l subsequently raise itself into geostationary | orbit by means of its onboard propulsion system. |
ficial satellite, Sputnik 1, had been put into | orbit by the Soviets in 1957, and this could be cons |
January 31 after a calculation of the comet's | orbit by Hidewo Hirose (Tokyo, Japan) after he took |
Soyuz capsule will be launched into low-earth | orbit by a Soyuz rocket. |
satellite, Explorer I, was confirmed to be in | orbit by the use of the phrase "Goldstone has the bi |
In 1968 it was taken into lunar | orbit by the Apollo 8 astronauts. |
It was launched into low Earth | orbit by a Falcon 1 rocket on July 14, 2009. |
struction by 2015 with manned missions to Mars | orbit by the mid-2030s. |
ched into an 817 km high polar sun synchronous | orbit by the eighth flight of India's Polar Satellit |
A's Mars Observer spacecraft into heliocentric | orbit, by means of a Transfer Orbit Stage. |
ng launch, it raised itself to a geostationary | orbit by means of its onboard SVM-5 apogee motor, at |
a Center catalogued 157 spacecraft placed into | orbit by launches which occurred in 1968. |
energy with Earth; this will alter Cruithne's | orbit by a little over half a million kilometres (wh |
star being eclipsed for about two days of each | orbit by HD 77581. |
to be raised to its operational geosynchronous | orbit by means of an Inertial Upper Stage, which con |
Both satellites were carried to | orbit by Delta 2914 rockets. |
one day by 1993 RP), and the first to have an | orbit calculated well enough to receive a number. |
dent in 1977, Dr. Butler learned techniques of | orbit calculation when he attended the Summer Scienc |
my with a curriculum based on observations and | orbit calculations of an asteroid. |
When the first parabolic | orbit calculations were made in 1886, there was a si |
he worked on such space technology problems as | orbit calculations, reentry paths, and space rendezv |
knowledged especially for his work in asteroid | orbit calculations, which brought him the Amateur Ac |
Kippes, acknowledged for his work in asteroid | orbit calculations. |
fundamental plane is the plane of the Earth's | orbit, called the ecliptic plane. |
headquarters, a hidden space station in Earth | orbit called Salvation III. |
is could not be done from the Gulf and a third | orbit, called Ethan Charlie, was created in Laos. |
The orbital speed at any position in the | orbit can be computed from the distance to the centr |
ermine various celestial parallax, and Earth's | orbit can be used for stellar parallax. |
Using this method, the inclination of the | orbit can be determined, revealing the planet's true |
No | orbit can be prepared from such limited data, but it |
However, the | orbit cannot be closed. |
ed: “Remote sensing images or photographs from | orbit cannot provide direct information about the or |
The inclination of this | orbit carries the star system as much as 0.75 kly (0 |
The inclination of its | orbit carries it as far as 90 parsecs above the gala |
car that extends up and down from his left eye | orbit, caused by a sharpened stick held by 7-year-ol |
termined from the slight wobble in the Earth's | orbit caused by the gravitational attraction of the |
n is beginning to cross a resonance in Earth's | orbit caused by the other planets. |
believed to measure 2.5 km in diameter, and to | orbit Celle at a distance of about 30 km. |
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