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 10096U 26022.50555830 +.00000000 +00000-0 +13759-3 0 00000
2 10096 75.8325 172.8650 0040318 115.5603 244.9767 14.91925779 07
| Epoch (UTC): | 22 January 2026 12:08:00 |
| Eccentricity: | 0.0040318 |
| inclination: | 75.8325° |
| perigee height: | 564 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 172.8650° |
| argument of perigee: | 115.5603° |
| revolutions per day: | 14.91925779 |
| mean anomaly at epoch: | 244.9767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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