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 25636U 26088.15341161 +.00000000 +00000-0 +68300-4 0 00002
2 25636 96.4804 343.7152 0140654 222.2308 136.7990 14.46432349 04
| Epoch (UTC): | 29 March 2026 03:40:54 |
| Eccentricity: | 0.0140654 |
| inclination: | 96.4804° |
| perigee height: | 637 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 343.7152° |
| argument of perigee: | 222.2308° |
| revolutions per day: | 14.46432349 |
| mean anomaly at epoch: | 136.7990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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