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 23091.43192555 .00008601 00000-0 77745-3 0 9990
2 32791 97.6483 64.3675 0010834 317.5497 42.4885 14.95648142810266
| Epoch (UTC): | 01 April 2023 10:21:58 |
| Eccentricity: | 0.0010834 |
| inclination: | 97.6483° |
| perigee height: | 573 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 64.3675° |
| argument of perigee: | 317.5497° |
| revolutions per day: | 14.95648142 |
| mean anomaly at epoch: | 42.4885° |
| orbit number at epoch: | 81026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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