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 35635U 26106.66895817 +.00000000 +00000-0 +21278-4 0 00004
2 35635 82.9542 73.9208 0020654 75.9743 96.4814 13.89945754 02
| Epoch (UTC): | 16 April 2026 16:03:17 |
| Eccentricity: | 0.0020654 |
| inclination: | 82.9542° |
| perigee height: | 914 km |
| apogee height: | 944 km |
| right ascension of ascending node: | 73.9208° |
| argument of perigee: | 75.9743° |
| revolutions per day: | 13.89945754 |
| mean anomaly at epoch: | 96.4814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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