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 26102.28728466 +.00000000 +00000-0 +85097-4 0 00000
2 36416 63.3863 222.9826 0693423 2.8772 357.5946 13.73043516 07
| Epoch (UTC): | 12 April 2026 06:53:41 |
| Eccentricity: | 0.0693423 |
| inclination: | 63.3863° |
| perigee height: | 478 km |
| apogee height: | 1499 km |
| right ascension of ascending node: | 222.9826° |
| argument of perigee: | 2.8772° |
| revolutions per day: | 13.73043516 |
| mean anomaly at epoch: | 357.5946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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