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 23080.88138228 .00002688 00000-0 50676-3 0 9998
2 28895 98.1383 213.7038 0015908 351.2143 8.8779 14.65255801928254
| Epoch (UTC): | 21 March 2023 21:09:11 |
| Eccentricity: | 0.0015908 |
| inclination: | 98.1383° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 213.7038° |
| argument of perigee: | 351.2143° |
| revolutions per day: | 14.65255801 |
| mean anomaly at epoch: | 8.8779° |
| orbit number at epoch: | 92825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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