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 26067.25271242 +.00000000 +00000-0 +32268-3 0 00009
2 23317 82.5375 351.3871 0014647 252.7729 107.1891 14.96875733 02
| Epoch (UTC): | 08 March 2026 06:03:54 |
| Eccentricity: | 0.0014647 |
| inclination: | 82.5375° |
| perigee height: | 566 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 351.3871° |
| argument of perigee: | 252.7729° |
| revolutions per day: | 14.96875733 |
| mean anomaly at epoch: | 107.1891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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