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 26129.52563558 +.00000000 +00000-0 +36383-4 0 00005
2 10096 75.8332 341.7309 0041090 201.7001 158.2453 14.92089019 09
| Epoch (UTC): | 09 May 2026 12:36:54 |
| Eccentricity: | 0.0041090 |
| inclination: | 75.8332° |
| perigee height: | 563 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 341.7309° |
| argument of perigee: | 201.7001° |
| revolutions per day: | 14.92089019 |
| mean anomaly at epoch: | 158.2453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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