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 51031U 22002AZ 23029.62987778 .00017542 00000-0 76426-3 0 9993
2 51031 97.4662 99.6236 0011523 0.3768 359.7475 15.22205352 57758
| Epoch (UTC): | 29 January 2023 15:07:01 |
| Eccentricity: | 0.0011523 |
| inclination: | 97.4662° |
| perigee height: | 491 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 99.6236° |
| argument of perigee: | 0.3768° |
| revolutions per day: | 15.22205352 |
| mean anomaly at epoch: | 359.7475° |
| orbit number at epoch: | 5775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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