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 36416U 26017.94200309 +.00000000 +00000-0 +13134-3 0 00001
2 36416 63.3883 92.3777 0685832 2.2945 358.0976 13.72763410 04
| Epoch (UTC): | 17 January 2026 22:36:29 |
| Eccentricity: | 0.0685832 |
| inclination: | 63.3883° |
| perigee height: | 484 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 92.3777° |
| argument of perigee: | 2.2945° |
| revolutions per day: | 13.72763410 |
| mean anomaly at epoch: | 358.0976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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