「orbit」の共起表現一覧(2語右で並び替え)
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| t had faded out of existence, but computed the | orbit for a very favorable 1973 apparition. |
| sity more than 1,000 times that of the Sun, an | orbit where a planet could be habitable would be loc |
| On the other hand, a putative companion would | orbit in a scorching region and would be as hot as a |
| For every one | orbit that a twotino makes, Neptune orbits 2 times. |
| It describes the construction and launch into | orbit of a sphere, 200 ft. in diameter, built of bri |
| It was operated in an | orbit with a perigee of 262 kilometres (163 mi), an |
| Following undocking, it remained in | orbit for a month, conducting an earth observation m |
| ble to put a 200,000 kg payload into low earth | orbit or a 67,000 kg payload into a translunar traje |
| their gravitational interaction causes them to | orbit about a common center of mass. |
| 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 |
| It was operated in an | orbit with a perigee of 265 kilometres (165 mi), an |
| he gravitational field of the Moon affects the | orbit of a spacecraft, it is possible to use these t |
| 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 |
| sions were initially put into an Earth parking | orbit as a launch platform with a rocket engine and |
| It was operated in an | orbit with a perigee of 211 kilometres (131 mi), an |
| conduct research at a 100-kilometer-high lunar | orbit as a preparation for a soft landing by Chang'e |
| 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 |
| It orbits the star in a slightly eccentric | orbit in a mean distance 20% further than Earth orbi |
| 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 |
| term, because spacecraft typically can't reach | orbit without a full fuel load. |
| It was operated in an | orbit with a perigee of 264 kilometres (164 mi), an |
| ing launch, it was positioned in geostationary | orbit at a longitude of 90° West for on-orbit testin |
| as launched on 15 November 1972 into low Earth | orbit with a periapsis of 443 km and an apoapsis of |
| Supersynchronous | orbit - A disposal / storage orbit above GSO/GEO. |
| It was operated in an | orbit with a perigee of 259 kilometres (161 mi), an |
| An elliptical | orbit with a period of about 400 years was calculate |
| 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 |
| Stella Tennant's career was catapulted into | orbit as a direct result of meeting Meisel, who imme |
| Kosmos 295 was operated in an | orbit with a perigee of 262 kilometres (163 mi), an |
| for a regular moon: if the | orbit of a planet's moon is highly inclined to the p |
| Discoverer 29 was operated in a low Earth | orbit, with a perigee of 138 kilometres (86 mi), an |
| ons of a surface feature and for computing the | orbit of a planet from three observations of its pos |
| Kosmos 497 was placed into a low Earth | orbit with a perigee of 271 kilometres (168 mi), an |
| Orbit was a founding member of the Association of Co | |
| hifting most of the "requirement for achieving | orbit to a robust ground infrastructure," intended t |
| PICOSat flies in a 800 km circular | orbit with a 67 degree inclination. |
| aunch, GOES 11 was positioned in geostationary | orbit at a longitude of 104° West for testing and on |
| n the Kuiper belt, but this radically modified | orbit implies a different and possibly extrasolar or |
| was to launch a very large hydrogen bomb into | orbit as a fractional orbital bombardment system (FO |
| the rocket, it manoeuvred into a geostationary | orbit with a perigee of 35,781 kilometres (22,233 mi |
| It was operated in an | orbit with a perigee of 190 kilometres (120 mi), an |
| For every one | orbit that a twotino makes, Neptune orbits twice. |
| s carrier rocket, Kosmos 36 was in a low Earth | orbit with a perigee of 253 kilometres (157 mi), an |
| An exchange | orbit is a where a pair of objects swap semimajor ax |
| 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 |
| Kosmos 521 was placed into a low Earth | orbit with a perigee of 987 kilometres (613 mi), an |
| ic variation of the eccentricity of the Moon's | orbit and a libration of similar period in the posit |
| 18 March 1965 it was catalogued as being in an | orbit with a perigee of 500 kilometres (270 nmi) and |
| It was operated in an | orbit with a perigee of 265 kilometres (165 mi), an |
| type Aten asteroid (meaning it crosses Earth's | orbit) and a Venus-crosser. |
| is intended to be positioned in geostationary | orbit at a longitude of 113º East, where it will rep |
| 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 |
| The | orbit has a period of 0.33381379 days and an inclina |
| It was operated in an | orbit with a perigee of 251 kilometres (156 mi), an |
| rated for the last time, the Agena remained in | orbit for a short time and was used to verify the co |
| The planetary | orbit is a circle |
| It was found to have a retrograde | orbit, at a very high angle of inclination to the pl |
| It was operated in an | orbit with a perigee of 214 kilometres (133 mi), an |
| e of placing a 4,000 kg payload into low Earth | orbit as a single-stage to orbit launch vehicle. |
| (54,000 mph), having likely been ejected from | orbit around a more massive star that was destroyed |
| ion which carried cosmonaut Gherman Titov into | orbit for a full day in order to study the effects o |
| ction satellites were lifted to geosynchronous | orbit by a fourth stage of a new, experimental desig |
| Kosmos 51 was placed into a low Earth | orbit with a perigee of 258 kilometres (160 mi), an |
| Polar | orbit - A satellite that passes above or nearly abov |
| 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 |
| of 2003 into a sun-synchronous 830 km circular | orbit at a local time of 0800-2000 UT. |
| It was operated in an | orbit with a perigee of 268 kilometres (167 mi), an |
| an expansion of the postorbital bone above the | orbit and a flange of the same bone inside the orbit |
| on July 17, 1991 into a Sun-synchronous polar | orbit at a height of 782-785 km. |
| 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 |
| It takes only 4.125 days (or 99 hours) to | orbit at a distance of 8.3 gigameters (0.0555 AU) aw |
| payload facilities are transported to and from | orbit using a carrier supplied by the ISS Program. |
| Kosmos 257 was operated in an | orbit with a perigee of 261 kilometres (162 mi), an |
| Areostationary | orbit is a concept similar to Earth's geostationary |
| It is positioned in geostationary | orbit at a longitude of 70 degrees East. |
| 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 |
| ous dynamical system corresponds to a periodic | orbit in a different but closely related dynamical s |
| A High Earth | Orbit is a geocentric orbit whose apogee lies above |
| 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 |
| at Yubileiny satellite which was launched into | orbit almost a year ago. |
| Arenstorf found a stable | orbit for a spacecraft orbiting between the Earth 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 |
| Haumea's | orbit has a slightly greater eccentricity than the o |
| 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 |
| cal mile (298 by 291 kilometres (181 mi)) high | orbit to a 140 nautical mile (259 kilometres (161 mi |
| The current best-fit circular | orbit has a period of 5.69 years, with a planetary m |
| 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 |
| d from an equatorial or high-inclination lunar | orbit to a polar landing site, along with bringing i |
| 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 |
| It is positioned in geostationary | orbit at a longitude of 119° West, from where it is |
| 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 planet's | orbit has a low eccentricity, similar to the planets |
| 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 |
| It was operated in an | orbit with a perigee of 388 kilometres (241 mi), an |
| It was operated in an | orbit with a perigee of 213 kilometres (132 mi), an |
| acean plane, as discussed here, relates to the | orbit of a planetary satellite. |
| 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 |
| The three CubeSats separated into low Earth | orbit during a coast phase of the launch, between th |
| 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 |
| and was thought to be located in an elliptical | orbit with a period of 264 days. |
| 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. |
| tal period is approximately 570 days, and they | orbit at a distance of approximately 4000 km (closes |
| Discoverer 36 was operated in a low Earth | orbit, with a perigee of 223 kilometres (139 mi), an |
| Soyuz capsule will be launched into low-earth | orbit by a Soyuz rocket. |
| 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 |
| 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 |
| of 3.15 AU and takes 4.9 years to complete the | orbit in a nearly circular path with an eccentricity |
| 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 |
| was tested against a US Air Force satellite in | orbit at a distance of 432 km (268 mi). |
| Maneuvering into a large circular | orbit, e.g. a geostationary orbit, requires a larger |
| observations have located the spacecraft in an | orbit with a perigee of 1,025 kilometres (637 mi) an |
| It travels a sun-synchronous | orbit, passing a given longitude at 10:30 AM local t |
| 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 |
| Haumea has a typical | orbit for a classical Kuiper belt object, with an or |
| Kosmos 750 was placed into a low Earth | orbit with a perigee of 272 kilometres (169 mi), an |
| concept of launching another Skylab into lunar | orbit using a spare S-IVB was briefly discussed arou |
| 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 |
| It was launched into low Earth | orbit by a Falcon 1 rocket on July 14, 2009. |
| system which contains a K0 I secondary star in | orbit around a primary star. |
| Kosmos 391 was placed into a low Earth | orbit with a perigee of 267 kilometres (166 mi), an |
| s Prime and Menda are diametrically opposed in | orbit around a vast Red Giant star. |
| Kosmos 31 was placed into a low Earth | orbit with a perigee of 221 kilometres (137 mi), an |
| It was operated in an | orbit with a perigee of 259 kilometres (161 mi), an |
| 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 |
| o far away that the Earth's movement along its | orbit makes a generally negligible difference to the |
| 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 |
| ientists, a mission would be placed in a polar | orbit for a month, from where it could observe the e |
| 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 |
| 73526 b was discovered orbiting its star in an | orbit just a little smaller than that of Venus' orbi |
| 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 |
| Kosmos 459 was placed into a low Earth | orbit with a perigee of 199 kilometres (124 mi), an |
| gai ☆ satellites, will separate into low Earth | orbit during a coast phase of the launch, between th |
| The | orbit of a spectroscopic binary is determined by mak |
| Kosmos 919 was placed into a low Earth | orbit with a perigee of 269 kilometres (167 mi), an |
| eached by a celestial body during its apparent | orbit around a given point of observation. |
| 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 |
| ime it entered service, it had already been in | orbit for a year past the end of its design life. |
| It was operated in an | orbit with a perigee of 220 kilometres (140 mi), an |
| ack hole would be if one actually observes the | orbit of a particle (or a blob of gas) that falls in |
| For every one | orbit that a twotino makes, Neptune orbits two times |
| It is the point in a star's | orbit around a galaxy when it lies closest to the ga |
| It was operated in an | orbit with a perigee of 265 kilometres (165 mi), an |
| Arabsat 1B was placed into a geosynchronous | orbit at a longitude of 26° East. |
| that will be used to propel it from low Earth | orbit onto a trajectory towards the Moon. |
| Kosmos 285 was operated in an | orbit with a perigee of 257 kilometres (160 mi), an |
| two stages that will propel it from low Earth | orbit to a trans-lunar trajectory. |
| Molniya | orbit is a type of highly elliptical orbit with an i |
| t exoplanet to be photographed, 2M1207b, is in | orbit around a star called 2M1207. |
| Explorer 2 failed to reach | orbit after a malfunction in the Jupiter-C launch ve |
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