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 31793U 07029B 23031.46375035 -.00000134 00000-0 -44747-4 0 9993
2 31793 70.9766 33.8521 0003096 272.1389 199.8508 14.14509427805103
| Epoch (UTC): | 31 January 2023 11:07:48 |
| Eccentricity: | 0.0003096 |
| inclination: | 70.9766° |
| perigee height: | 842 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 33.8521° |
| argument of perigee: | 272.1389° |
| revolutions per day: | 14.14509427 |
| mean anomaly at epoch: | 199.8508° |
| orbit number at epoch: | 80510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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