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 22081U 92053B 22144.77996490 .00000197 00000-0 80174-4 0 9997
2 22081 74.0460 23.4471 0036907 271.1315 88.5608 14.33608104556654
| Epoch (UTC): | 24 May 2022 18:43:08 |
| Eccentricity: | 0.0036907 |
| inclination: | 74.0460° |
| perigee height: | 753 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 23.4471° |
| argument of perigee: | 271.1315° |
| revolutions per day: | 14.33608104 |
| mean anomaly at epoch: | 88.5608° |
| orbit number at epoch: | 55665 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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