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 23705U 26017.89323279 +.00000000 +00000-0 -44162-4 0 00001
2 23705 71.0223 286.9017 0013521 207.2599 152.7816 14.15489957 06
| Epoch (UTC): | 17 January 2026 21:26:15 |
| Eccentricity: | 0.0013521 |
| inclination: | 71.0223° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 286.9017° |
| argument of perigee: | 207.2599° |
| revolutions per day: | 14.15489957 |
| mean anomaly at epoch: | 152.7816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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