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 23608U 26017.89601777 +.00000000 +00000-0 +72093-3 0 00007
2 23608 98.2884 214.9791 0007189 214.7779 145.2997 15.42918496 01
| Epoch (UTC): | 17 January 2026 21:30:15 |
| Eccentricity: | 0.0007189 |
| inclination: | 98.2884° |
| perigee height: | 433 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 214.9791° |
| argument of perigee: | 214.7779° |
| revolutions per day: | 15.42918496 |
| mean anomaly at epoch: | 145.2997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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