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 10011U 26071.99663720 +.00000000 +00000-0 -10222-3 0 00005
2 10011 65.8627 278.7078 0692240 73.6524 71.3357 12.32266690 01
| Epoch (UTC): | 12 March 2026 23:55:09 |
| Eccentricity: | 0.0692240 |
| inclination: | 65.8627° |
| perigee height: | 991 km |
| apogee height: | 2088 km |
| right ascension of ascending node: | 278.7078° |
| argument of perigee: | 73.6524° |
| revolutions per day: | 12.32266690 |
| mean anomaly at epoch: | 71.3357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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