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 23161.13741691 .00000299 00000-0 18066-3 0 9990
2 31793 70.9749 121.4138 0001682 274.0036 96.7952 14.14538345823537
| Epoch (UTC): | 10 June 2023 03:17:52 |
| Eccentricity: | 0.0001682 |
| inclination: | 70.9749° |
| perigee height: | 842 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 121.4138° |
| argument of perigee: | 274.0036° |
| revolutions per day: | 14.14538345 |
| mean anomaly at epoch: | 96.7952° |
| orbit number at epoch: | 82353 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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