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 42789U 17036AA 23316.24878152 .15089340 24242-5 33245-3 0 9998
2 42789 97.0967 358.2701 0009105 256.4814 103.5475 16.46095853356311
| Epoch (UTC): | 12 November 2023 05:58:14 |
| Eccentricity: | 0.0009105 |
| inclination: | 97.0967° |
| perigee height: | 144 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 358.2701° |
| argument of perigee: | 256.4814° |
| revolutions per day: | 16.46095853 |
| mean anomaly at epoch: | 103.5475° |
| orbit number at epoch: | 35631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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