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 22022.00558311 .00000114 00000-0 14678-3 0 9998
2 00016 34.2637 269.6746 2026603 178.2650 182.6409 10.48800609520106
| Epoch (UTC): | 22 January 2022 00:08:02 |
| Eccentricity: | 0.2026603 |
| inclination: | 34.2637° |
| perigee height: | 651 km |
| apogee height: | 4224 km |
| right ascension of ascending node: | 269.6746° |
| argument of perigee: | 178.2650° |
| revolutions per day: | 10.48800609 |
| mean anomaly at epoch: | 182.6409° |
| orbit number at epoch: | 52010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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