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 is defined by the following mean orbital elements,
1 23751U 26020.97319316 +.00000000 +00000-0 +12945-3 0 00004
2 23751 99.0300 36.2406 0001088 84.8103 275.3198 14.23522985 09
| Epoch (UTC): | 20 January 2026 23:21:23 |
| Eccentricity: | 0.0001088 |
| inclination: | 99.0300° |
| perigee height: | 813 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 36.2406° |
| argument of perigee: | 84.8103° |
| revolutions per day: | 14.23522985 |
| mean anomaly at epoch: | 275.3198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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