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 26022.45841455 +.00000000 +00000-0 +29733-3 0 00008
2 36416 63.3880 80.0993 0686163 2.3268 358.0696 13.72777875 01
| Epoch (UTC): | 22 January 2026 11:00:07 |
| Eccentricity: | 0.0686163 |
| inclination: | 63.3880° |
| perigee height: | 484 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 80.0993° |
| argument of perigee: | 2.3268° |
| revolutions per day: | 13.72777875 |
| mean anomaly at epoch: | 358.0696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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