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 16591U 86014A 22361.66195355 0.00013300 00000-0 74174-3 0 01
2 16591 63.3484 219.0446 0910250 87.3190 272.6810 13.61625463 06
| Epoch (UTC): | 27 December 2022 15:53:12 |
| Eccentricity: | 0.0910250 |
| inclination: | 63.3484° |
| perigee height: | 355 km |
| apogee height: | 1704 km |
| right ascension of ascending node: | 219.0446° |
| argument of perigee: | 87.3190° |
| revolutions per day: | 13.61625463 |
| mean anomaly at epoch: | 272.6810° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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