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 16496U 86006B 23159.41425840 .00000632 00000-0 71518-4 0 9991
2 16496 82.5238 124.1616 0020666 67.2553 47.9058 14.84707049999931
| Epoch (UTC): | 08 June 2023 09:56:31 |
| Eccentricity: | 0.0020666 |
| inclination: | 82.5238° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 124.1616° |
| argument of perigee: | 67.2553° |
| revolutions per day: | 14.84707049 |
| mean anomaly at epoch: | 47.9058° |
| orbit number at epoch: | 99993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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