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 25341.03587860 .00000453 00000-0 16773-3 0 9993
2 22081 74.0417 179.4902 0034403 110.9428 249.5412 14.34755810741905
| Epoch (UTC): | 07 December 2025 00:51:39 |
| Eccentricity: | 0.0034403 |
| inclination: | 74.0417° |
| perigee height: | 751 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 179.4902° |
| argument of perigee: | 110.9428° |
| revolutions per day: | 14.34755810 |
| mean anomaly at epoch: | 249.5412° |
| orbit number at epoch: | 74190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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