A geocentric orbit involves any object orbiting the Earth, such as the Moon or artificial satellites. Currently there are approximately 2,465 artificial satellites orbiting the Earth and 6,216 pieces of space debris as tracked by the Goddard Space Flight Center. Over 16,291 previously launched objects have decayed into the Earth's atmosphere.
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The following is a list of different geocentric orbit classifications.
| orbit | center-to-center distance |
altitude above the Earth's surface |
speed | period/time in space | specific orbital energy |
|---|---|---|---|---|---|
| minimum sub-orbital spaceflight (vertical) | 6,500 km | 100 km | 0.0 km/s | just reaching space | 1.0 MJ/kg |
| ICBM | up to 7,600 km | up to 1,200 km | 6 to 7 km/s | time in space: 25 min | 27 MJ/kg |
| Low Earth orbit | 6,600 to 8,400 km | 200 to 2,000 km | circular orbit: 6.9 to 7.8 km/s elliptic orbit: 6.5 to 8.2 km/s |
89 to 128 min | 32.1 to 38.6 MJ/kg |
| Molniya orbit | 6,900 to 46,300 km | 500 to 39,900 km | 1.5 to 10.0 km/s | 11 h 58 min | 54.8 MJ/kg |
| GEO | 42,000 km | 35,786 km | 3.1 km/s | 23 h 56 min | 57.5 MJ/kg |
| Orbit of the Moon | 363,000 to 406,000 km | 357,000 to 399,000 km | 0.97 to 1.08 km/s | 27.3 days | 61.8 MJ/kg |
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