「ORBIT」の共起表現一覧(1語右で並び替え)11ページ目
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It travels in a highly eccentric | orbit which has a perihelion (closest approach to th |
+2.80 to +3.08 over the course of the binary's | orbit, which takes 1.4402 days to complete. |
th an unusual, almost perpendicular retrograde | orbit which brings it into the inner solar system by |
derian gland is a gland found within the eye's | orbit which occurs in vertebrates (reptiles, amphibi |
quent flights, the landing occurred during the | orbit which provided the nominal launch opportunity. |
st Silvio Berlusconi, to return into the PdL's | orbit, while Menia remained firmly behind Fini. |
In a spacecraft, this is an | orbit, while for aircraft it is their landing locati |
for maximum flexibility to ensure delivery to | orbit while allowing the Alliance's three members to |
rvice Module (CSM) remained in a lunar parking | orbit while the Lunar Module (LM) landed. |
ission, STS-82, to re-boost Hubble to a higher | orbit while still in orbiter payload bay. |
ination of 0° or 180° corresponds to a face-on | orbit, while an inclination of 90° corresponds to an |
ked, such as raising or lowering the station's | orbit, whilst the remaining 502 kilograms (1,110 lb) |
William | Orbit Widescreen Mix (6:33) |
Late in the mission, the | orbit will be lowered to an elliptical one with the |
The parameters of the osculating Kepler | orbit will then only slowly change and the osculatin |
Ideally, every gauge | orbit will intersect this submanifold once and only |
cial satellite, to increase the time until its | orbit will decay and it re-enters the atmosphere. |
perturbing (non-Keplarian) forces on an actual | orbit will cause the osculating eccentricity vector |
The launch of its own satellite on | orbit will be Azerbaijan's first action in realizing |
in different directions are commensurate, the | orbit will lie on a one- or two-dimensional manifold |
Further observations of the | orbit will be required. |
tellite that is in (a prograde) subsynchronous | orbit will appear to drift eastward as seen from the |
The | orbit will continue to decay and eventually the stag |
The lengths of its | orbit will oscillate slightly above and below the 2: |
oint, however, this trend will reverse and its | orbit will increase. |
This | orbit will carry the system as close as 17.4 kly (5. |
The inclination of this | orbit will carry the stars as much as 1.3 kly (0.4 k |
next close encounter of 2009 DD45 with Earth's | orbit will be in 2067. |
he asteroid were quickly found and the present | orbit will take the asteroid past the Earth on Octob |
for a while, make dimmer) the stars that they | orbit with respect to Earth. |
It was operated in an | orbit with a perigee of 262 kilometres (163 mi), an |
edae caused by the planet's gravity during its | orbit with the Doppler spectroscopy. |
loser to the Sun and Earth can have Mars's old | orbit, with a hydrogen bomb being used to blow Earth |
A trojan object shares an | orbit with a larger object, but does not collide wit |
Ariel 6 operated in an | orbit with an apogee of 651 kilometres (405 mi), a p |
It was operated in an | orbit with a perigee of 265 kilometres (165 mi), an |
Kosmos 283 was operated in an | orbit with a perigee of 196 kilometres (122 mi), an |
FASTSAT was deployed into a low Earth | orbit with a perigee of 650 kilometers (400 mi), an |
d Lewis was successfully placed into a parking | orbit with an apogee of 134 kilometres (83 mi), a pe |
It was operated in an | orbit with a perigee of 211 kilometres (131 mi), an |
Kosmos 245 was operated in an | orbit with a perigee of 260 kilometres (160 mi), an |
year 2200, the comet will have a centaur-like | orbit with a perihelion (closest distance to the Sun |
It was operated in an | orbit with a perigee of 268 kilometres (167 mi), an |
observations verified the satellite was in an | orbit with a period of almost 24 hours at a 33° incl |
It was operated in an | orbit with a perigee of 268 kilometres (167 mi), an |
The pair | orbit with a period of 22,423 days (61.4 years) and |
It was operated in an | orbit with a perigee of 233 kilometres (145 mi), an |
It was operated in an | orbit with a perigee of 264 kilometres (164 mi), an |
as launched on 15 November 1972 into low Earth | orbit with a periapsis of 443 km and an apoapsis of |
It was operated in an | orbit with a perigee of 259 kilometres (161 mi), an |
d resulted in Explorer 9 being deployed into a | orbit with an apogee of 2,581 kilometres (1,604 mi), |
An elliptical | orbit with a period of about 400 years was calculate |
The inclination of Mars' | orbit with respect to Saturn's ecliptic is 2.36°, wh |
It was operated in an | orbit with a perigee of 197 kilometres (122 mi), an |
It was operated in an | orbit with a perigee of 147 kilometres (91 mi), an a |
Kosmos 394 was placed into a low Earth | orbit with a perigee of 522 kilometres (324 mi), an |
It was operated in an | orbit with a perigee of 264 kilometres (164 mi), an |
It operates in a Molniya | orbit with a perigee of 900 kilometres (560 mi), an |
Kosmos 295 was operated in an | orbit with a perigee of 262 kilometres (163 mi), an |
Discoverer 29 was operated in a low Earth | orbit, with a perigee of 138 kilometres (86 mi), an |
Kosmos 497 was placed into a low Earth | orbit with a perigee of 271 kilometres (168 mi), an |
Placed into an | orbit with an apogee of 185,000 kilometres (115,000 |
PICOSat flies in a 800 km circular | orbit with a 67 degree inclination. |
the rocket, it manoeuvred into a geostationary | orbit with a perigee of 35,781 kilometres (22,233 mi |
rated from its carrier rocket into a low Earth | orbit with an apogee of 445 kilometres (277 mi), a p |
resonance to the 5:2 resonance with Jupiter's | orbit with dynamical lifetimes of 1-100 Ma. |
It was operated in an | orbit with a perigee of 190 kilometres (120 mi), an |
as launched on May 17, 1968, had an elliptical | orbit with initially apogee of 1086 km, perigee 326 |
s carrier rocket, Kosmos 36 was in a low Earth | orbit with a perigee of 253 kilometres (157 mi), an |
It was left in an | orbit with a perigee of 421 kilometres (262 mi), an |
an angle of 6.6 arcseconds, which indicates an | orbit with a semimajor axis whose expected value is |
Kosmos 26 was placed into a low Earth | orbit with a perigee of 268 kilometres (167 mi), an |
f the spacecraft after just over seven days in | orbit, with the orbital module staying in orbit for |
Kosmos 521 was placed into a low Earth | orbit with a perigee of 987 kilometres (613 mi), an |
18 March 1965 it was catalogued as being in an | orbit with a perigee of 500 kilometres (270 nmi) and |
Six other Little Pocket Mice were sent into | orbit with Skylab 3 in July 1973, though these anima |
It was operated in an | orbit with a perigee of 265 kilometres (165 mi), an |
Discoverer 32 was operated in a low Earth | orbit, with a perigee of 233 kilometres (145 mi), an |
Discoverer 19 was operated in a low Earth | orbit, with a perigee of 206 kilometres (128 mi), an |
Kosmos 1241 was placed into a low Earth | orbit with a perigee of 989 kilometres (615 mi), an |
/2000 U5 had a barycentric (epoch 1960-Jan-01) | orbit with an apoapsis distance of 5,473 AU, and a p |
It was operated in an | orbit with a perigee of 251 kilometres (156 mi), an |
e 29, 2004 on a quasi Sun-synchronous circular | orbit with an inclination of about 98.23° and an alt |
erbolic trajectory, in order to bring it in an | orbit with an eccentricity of less than 1. |
It was operated in an | orbit with a perigee of 214 kilometres (133 mi), an |
Kosmos 51 was placed into a low Earth | orbit with a perigee of 258 kilometres (160 mi), an |
In 9 minutes, the vehicle reached low earth | orbit with the following parameters: min altitude - |
Kosmos 19 was placed into a low Earth | orbit with a perigee of 267 kilometres (166 mi), an |
It was operated in an | orbit with a perigee of 208 kilometres (129 mi), an |
The satellite separated into an | orbit with an apogee of 699.9 kilometres (434.9 mi), |
It was operated in an | orbit with a perigee of 268 kilometres (167 mi), an |
ce of aliens once occupied a planet sharing an | orbit with the asteroid belt. |
Kosmos 311 was operated in an | orbit with a perigee of 263 kilometres (163 mi), an |
It was operated in an | orbit with a perigee of 267 kilometres (166 mi), an |
e Procerus, joining at the medial angle of the | orbit with the infratrochlear and nasociliary branch |
ecraft launched from Wallops Island to achieve | orbit, with one previous attempt having failed. |
BeeSat-1 is operating in a sun synchronous | orbit with an apogee of 723 kilometres (449 mi), a p |
Kosmos 257 was operated in an | orbit with a perigee of 261 kilometres (162 mi), an |
rated from its carrier rocket into a low Earth | orbit with an apogee of 510 kilometres (320 mi), a p |
It was operated in an | orbit with a perigee of 158 kilometres (98 mi), an a |
Kosmos 1375 was placed into a low Earth | orbit with a perigee of 986 kilometres (613 mi), an |
t effort to build a rocket capable of reaching | orbit with a commercial payload. |
as launched on 27 September 2003 into an Earth | orbit with a height between 675 and 695 km. |
Kosmos 233 was operated in an | orbit with a perigee of 198 kilometres (123 mi), an |
It was operated in an | orbit with a perigee of 197 kilometres (122 mi), an |
Kosmos 11 was placed into a low Earth | orbit with a perigee of 240 kilometres (150 mi), an |
Kosmos 440 was placed into a low Earth | orbit with a perigee of 272 kilometres (169 mi), an |
It was operated in an | orbit with a perigee of 226 kilometres (140 mi), an |
Kosmos 49 was placed into a low Earth | orbit with a perigee of 260 kilometres (160 mi), an |
Kosmos 4 was placed into a low Earth | orbit with a perigee of 285 kilometres (177 mi), an |
a 58.8 by 9.5 nautical mile (108.9 by 17.6 km) | orbit, with the low point over Hadley Rille landing |
Kosmos 615 was placed into a low Earth | orbit with a perigee of 270 kilometres (170 mi), an |
Kosmos 308 was placed into a low Earth | orbit with a perigee of 271 kilometres (168 mi), an |
understood to describe satellites in low Earth | orbit with respect to the sun (the solar vector). |
It takes about 33 months to | orbit with semi-amplitude of 17.9 m/s. |
It ended up in a low Earth | orbit with a perigee of 167 kilometres (104 mi), an |
No unaccelerated | orbit with a semi-major axis less than this distance |
the rocket, it manoeuvred into a geostationary | orbit with a perigee of 35,785 kilometres (22,236 mi |
Discoverer 25 was operated in a low Earth | orbit, with a perigee of 223 kilometres (139 mi), an |
It was operated in an | orbit with a perigee of 266 kilometres (165 mi), an |
space craft entering the base's gravitational | orbit with the game play changing from a first perso |
It was operated in an | orbit with a perigee of 388 kilometres (241 mi), an |
the magnetic field of a giant planet in tight | orbit with that star's own magnetic field. |
It was operated in an | orbit with a perigee of 213 kilometres (132 mi), an |
It was operated in an | orbit with a perigee of 264 kilometres (164 mi), an |
e LM began its landing sequence with a descent | orbit with a perilune of about 50,000 feet (15 km; 8 |
It was operated in an | orbit with a perigee of 258 kilometres (160 mi), an |
Kosmos 191 was operated in an | orbit with a perigee of 261 kilometres (162 mi), an |
It was operated in an | orbit with a perigee of 262 kilometres (163 mi), an |
Ariel 2 was placed into a low Earth | orbit, with a perigee of 289 kilometres (180 mi), an |
Discoverer 34 was launched into a low Earth | orbit, with a perigee of 225 kilometres (140 mi), an |
uroral probe was launched August 29, 1996 into | orbit with an apogee of 20 000 km. |
and was thought to be located in an elliptical | orbit with a period of 264 days. |
tail probe was launched August 3, 1995 into | orbit with an apogee of 200 000 km; |
Kosmos 1 was placed into a low Earth | orbit with a perigee of 207 kilometres (129 mi), an |
Johann Franz Encke determined a definitive | orbit with a period of 70.68 years. |
Discoverer 36 was operated in a low Earth | orbit, with a perigee of 223 kilometres (139 mi), an |
It was operated in an | orbit with a perigee of 266 kilometres (165 mi), an |
Kosmos 275 was placed into a low Earth | orbit with a perigee of 273 kilometres (170 mi), an |
e Counter-Earth followed the Earth on the same | orbit with half a year of delay, it would sometimes |
Kosmos 176 was operated in an | orbit with a perigee of 193 kilometres (120 mi), an |
It was operated in an | orbit with a perigee of 263 kilometres (163 mi), an |
This planet orbits in a highly eccentric | orbit with a semi-major axis of 1.36 AU. |
Kosmos 268 was operated in an | orbit with a perigee of 212 kilometres (132 mi), an |
the star, taking only 18 days to complete its | orbit with average speed of 86.5 km/s. |
It is currently in a geostationary | orbit, with an apogee of 35,788 kilometres (22,238 m |
observations have located the spacecraft in an | orbit with a perigee of 1,025 kilometres (637 mi) an |
It was operated in an | orbit with a perigee of 268 kilometres (167 mi), an |
Kosmos 3 was placed into a low Earth | orbit with a perigee of 204 kilometres (127 mi), an |
Mercury also has an elliptical | orbit, with an eccentricity of .2056. |
SwissCube-1 is operating in a sun synchronous | orbit with an apogee of 752 kilometres (467 mi), a p |
Kosmos 750 was placed into a low Earth | orbit with a perigee of 272 kilometres (169 mi), an |
Kosmos 221 was operated in an | orbit with a perigee of 214 kilometres (133 mi), an |
It was operated in an | orbit with a perigee of 237 kilometres (147 mi), an |
It was operated in an | orbit with a perigee of 261 kilometres (162 mi), an |
It was operated in an | orbit with a perigee of 256 kilometres (159 mi), an |
It was operated in an | orbit with a perigee of 266 kilometres (165 mi), an |
Kosmos 391 was placed into a low Earth | orbit with a perigee of 267 kilometres (166 mi), an |
Kosmos 31 was placed into a low Earth | orbit with a perigee of 221 kilometres (137 mi), an |
onfiguration could launch 4,790 kg to the same | orbit with four liquid boosters added . |
It was operated in an | orbit with a perigee of 259 kilometres (161 mi), an |
ly written by and recorded by Beck and William | Orbit with the intention of being a Beck track, but |
Kosmos 277 was operated in an | orbit with a perigee of 256 kilometres (159 mi), an |
Kosmos 265 was operated in an | orbit with a perigee of 261 kilometres (162 mi), an |
Kosmos 901 was placed into a low Earth | orbit with a perigee of 269 kilometres (167 mi), an |
The inclination of Mercury's | orbit with respect to that of Mars is 5.16°, which i |
It was operated in an | orbit with a perigee of 266 kilometres (165 mi), an |
Kosmos 211 was operated in an | orbit with a perigee of 197 kilometres (122 mi), an |
Kosmos 803 was placed into a low Earth | orbit with a perigee of 505 kilometres (314 mi), an |
around which an extrasolar planet is known to | orbit with a mean distance from the central star sli |
It was operated in an | orbit with a perigee of 267 kilometres (166 mi), an |
It was operated in an | orbit with a perigee of 266 kilometres (165 mi), an |
rated from the carrier rocket into a low Earth | orbit with an apogee of 490 kilometres (300 mi), a p |
Kosmos 222 was operated in an | orbit with a perigee of 259 kilometres (161 mi), an |
Kosmos 106 was placed into a low Earth | orbit with a perigee of 281 kilometres (175 mi), an |
Kosmos 70 was placed into a low Earth | orbit with a perigee of 223 kilometres (139 mi), an |
rated from its carrier rocket into a low Earth | orbit with an apogee of 444 kilometres (276 mi), a p |
ATDA in | orbit, with its payload fairing still attached. |
Kosmos 459 was placed into a low Earth | orbit with a perigee of 199 kilometres (124 mi), an |
Kosmos 919 was placed into a low Earth | orbit with a perigee of 269 kilometres (167 mi), an |
The inclination of Mercury's | orbit with respect to Saturn's ecliptic is 6.38°, wh |
n orbits the nucleus and its smallest possible | orbit, with lowest energy, is called the Bohr radius |
It was operated in an | orbit with a perigee of 267 kilometres (166 mi), an |
Discoverer 26 was operated in a low Earth | orbit, with a perigee of 229 kilometres (142 mi), an |
Kosmos 303 was operated in an | orbit with a perigee of 259 kilometres (161 mi), an |
arge distance, using a polar highly elliptical | orbit with its apogee above that area. |
It was operated in an | orbit with a perigee of 220 kilometres (140 mi), an |
progresses the two boys drift further into his | orbit, with unsettling results. |
It was operated in an | orbit with a perigee of 265 kilometres (165 mi), an |
Kosmos 285 was operated in an | orbit with a perigee of 257 kilometres (160 mi), an |
It was operated in an | orbit with a perigee of 263 kilometres (163 mi), an |
to determine the parameters of the satellite's | orbit with a greater degree of precision. |
Kosmos 662 was placed into a low Earth | orbit with a perigee of 271 kilometres (168 mi), an |
The craft is in a nearly circular | orbit with an eccentricity of 0.028, and having lost |
It was operated in an | orbit with a perigee of 277 kilometres (172 mi), an |
It was operated in an | orbit with a perigee of 256 kilometres (159 mi), an |
Kosmos 173 was operated in an | orbit with a perigee of 261 kilometres (162 mi), an |
Kosmos 849 was placed into a low Earth | orbit with a perigee of 264 kilometres (164 mi), an |
These two stars have an | orbit with a semi-major axis of 3.4″, which is appro |
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