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 22236U 92080A 25350.96547008 .00001869 00000-0 16487-3 0 9991
2 22236 82.5040 358.2807 0016225 108.7533 251.5451 14.95777119768423
| Epoch (UTC): | 16 December 2025 23:10:16 |
| Eccentricity: | 0.0016225 |
| inclination: | 82.5040° |
| perigee height: | 568 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 358.2807° |
| argument of perigee: | 108.7533° |
| revolutions per day: | 14.95777119 |
| mean anomaly at epoch: | 251.5451° |
| orbit number at epoch: | 76842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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