View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 22220U 92076B 24278.93223671 .00000585 00000-0 31637-3 0 9999
2 22220 71.0003 205.2347 0012639 179.2466 247.5365 14.16709016648072
| Epoch (UTC): | 04 October 2024 22:22:25 |
| Eccentricity: | 0.0012639 |
| inclination: | 71.0003° |
| perigee height: | 827 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 205.2347° |
| argument of perigee: | 179.2466° |
| revolutions per day: | 14.16709016 |
| mean anomaly at epoch: | 247.5365° |
| orbit number at epoch: | 64807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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