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 26076.28631138 +.00000000 +00000-0 +16680-3 0 00000
2 36416 63.3865 293.7189 0690775 2.6994 357.7478 13.73002253 03
| Epoch (UTC): | 17 March 2026 06:52:17 |
| Eccentricity: | 0.0690775 |
| inclination: | 63.3865° |
| perigee height: | 480 km |
| apogee height: | 1498 km |
| right ascension of ascending node: | 293.7189° |
| argument of perigee: | 2.6994° |
| revolutions per day: | 13.73002253 |
| mean anomaly at epoch: | 357.7478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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