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 32791U 08021J 23155.63618636 .00004690 00000-0 41632-3 0 9996
2 32791 97.6548 127.1382 0013696 93.5485 266.7304 14.96564485819789
| Epoch (UTC): | 04 June 2023 15:16:06 |
| Eccentricity: | 0.0013696 |
| inclination: | 97.6548° |
| perigee height: | 568 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 127.1382° |
| argument of perigee: | 93.5485° |
| revolutions per day: | 14.96564485 |
| mean anomaly at epoch: | 266.7304° |
| orbit number at epoch: | 81978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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