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 23088.88960217 .00010814 00000-0 97710-3 0 9996
2 32791 97.6495 61.8862 0010957 327.7038 32.3511 14.95596704809885
| Epoch (UTC): | 29 March 2023 21:21:01 |
| Eccentricity: | 0.0010957 |
| inclination: | 97.6495° |
| perigee height: | 573 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 61.8862° |
| argument of perigee: | 327.7038° |
| revolutions per day: | 14.95596704 |
| mean anomaly at epoch: | 32.3511° |
| orbit number at epoch: | 80988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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