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 26106.65712904 +.00000000 +00000-0 +73363-4 0 00008
2 36416 63.3861 211.0944 0693886 2.9101 357.5663 13.73047163 03
| Epoch (UTC): | 16 April 2026 15:46:15 |
| Eccentricity: | 0.0693886 |
| inclination: | 63.3861° |
| perigee height: | 477 km |
| apogee height: | 1500 km |
| right ascension of ascending node: | 211.0944° |
| argument of perigee: | 2.9101° |
| revolutions per day: | 13.73047163 |
| mean anomaly at epoch: | 357.5663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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