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 28895U 05043F 24262.34315866 .00005720 00000-0 99115-3 0 9998
2 28895 98.2148 38.4146 0016070 65.2224 295.0651 14.68586305 8122
| Epoch (UTC): | 18 September 2024 08:14:08 |
| Eccentricity: | 0.0016070 |
| inclination: | 98.2148° |
| perigee height: | 654 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 38.4146° |
| argument of perigee: | 65.2224° |
| revolutions per day: | 14.68586305 |
| mean anomaly at epoch: | 295.0651° |
| orbit number at epoch: | 812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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