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 26158.75622573 +.00000000 +00000-0 +19166-3 0 00004
2 23317 82.5335 263.9743 0014969 308.7808 51.2077 14.97215180 01
| Epoch (UTC): | 07 June 2026 18:08:57 |
| Eccentricity: | 0.0014969 |
| inclination: | 82.5335° |
| perigee height: | 565 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 263.9743° |
| argument of perigee: | 308.7808° |
| revolutions per day: | 14.97215180 |
| mean anomaly at epoch: | 51.2077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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