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 00016U 58002A 23342.52182289 .00000378 00000-0 51900-3 0 9999
2 00016 34.2645 89.9221 2020716 189.2702 166.4308 10.48992682592082
| Epoch (UTC): | 08 December 2023 12:31:25 |
| Eccentricity: | 0.2020716 |
| inclination: | 34.2645° |
| perigee height: | 655 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 89.9221° |
| argument of perigee: | 189.2702° |
| revolutions per day: | 10.48992682 |
| mean anomaly at epoch: | 166.4308° |
| orbit number at epoch: | 59208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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