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 2142U 66031A 24357.62232746 .00000328 00000-0 12163-3 0 9997
2 2142 35.0468 50.3839 0006845 4.2468 355.8277 14.34456761 73695
| Epoch (UTC): | 22 December 2024 14:56:09 |
| Eccentricity: | 0.0006845 |
| inclination: | 35.0468° |
| perigee height: | 772 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 50.3839° |
| argument of perigee: | 4.2468° |
| revolutions per day: | 14.34456761 |
| mean anomaly at epoch: | 355.8277° |
| orbit number at epoch: | 7369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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