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 23317U 26041.91620478 +.00000000 +00000-0 +24522-3 0 00007
2 23317 82.5343 15.5729 0015997 345.8176 14.2594 14.96729116 08
| Epoch (UTC): | 10 February 2026 21:59:20 |
| Eccentricity: | 0.0015997 |
| inclination: | 82.5343° |
| perigee height: | 566 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 15.5729° |
| argument of perigee: | 345.8176° |
| revolutions per day: | 14.96729116 |
| mean anomaly at epoch: | 14.2594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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