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 10962U 26071.50671649 +.00000000 +00000-0 +13109-3 0 00002
2 10962 74.0761 84.8677 0026093 246.7843 113.0566 14.42846557 07
| Epoch (UTC): | 12 March 2026 12:09:40 |
| Eccentricity: | 0.0026093 |
| inclination: | 74.0761° |
| perigee height: | 731 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 84.8677° |
| argument of perigee: | 246.7843° |
| revolutions per day: | 14.42846557 |
| mean anomaly at epoch: | 113.0566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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