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 26075.20746911 +.00000000 +00000-0 +19277-3 0 00008
2 23317 82.5376 343.7935 0015029 223.1788 136.8257 14.96915766 07
| Epoch (UTC): | 16 March 2026 04:58:45 |
| Eccentricity: | 0.0015029 |
| inclination: | 82.5376° |
| perigee height: | 566 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 343.7935° |
| argument of perigee: | 223.1788° |
| revolutions per day: | 14.96915766 |
| mean anomaly at epoch: | 136.8257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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