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 26020.56444176 +.00000000 +00000-0 +26731-3 0 00002
2 36416 63.3883 85.2484 0686024 2.3125 358.0820 13.72771794 07
| Epoch (UTC): | 20 January 2026 13:32:47 |
| Eccentricity: | 0.0686024 |
| inclination: | 63.3883° |
| perigee height: | 484 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 85.2484° |
| argument of perigee: | 2.3125° |
| revolutions per day: | 13.72771794 |
| mean anomaly at epoch: | 358.0820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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