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 26071.19669225 +.00000000 +00000-0 +21472-3 0 00004
2 23317 82.5373 347.6224 0014884 237.9186 122.0592 14.96898340 08
| Epoch (UTC): | 12 March 2026 04:43:14 |
| Eccentricity: | 0.0014884 |
| inclination: | 82.5373° |
| perigee height: | 566 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 347.6224° |
| argument of perigee: | 237.9186° |
| revolutions per day: | 14.96898340 |
| mean anomaly at epoch: | 122.0592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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