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 20580U 90037B 23031.55986403 .00003761 00000-0 20410-3 0 9990
2 20580 28.4705 96.1763 0002151 351.6418 117.9489 15.11804083600750
| Epoch (UTC): | 31 January 2023 13:26:12 |
| Eccentricity: | 0.0002151 |
| inclination: | 28.4705° |
| perigee height: | 529 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 96.1763° |
| argument of perigee: | 351.6418° |
| revolutions per day: | 15.11804083 |
| mean anomaly at epoch: | 117.9489° |
| orbit number at epoch: | 60075 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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