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 28594U 79095E 23089.91265320 .00011908 00000-0 44606-2 0 9999
2 28594 81.2026 164.8134 0016981 42.3734 317.8756 14.31567535964684
| Epoch (UTC): | 30 March 2023 21:54:13 |
| Eccentricity: | 0.0016981 |
| inclination: | 81.2026° |
| perigee height: | 774 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 164.8134° |
| argument of perigee: | 42.3734° |
| revolutions per day: | 14.31567535 |
| mean anomaly at epoch: | 317.8756° |
| orbit number at epoch: | 96468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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