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 26107.93853178 +.00000000 +00000-0 +37129-4 0 00001
2 25636 96.4777 358.8658 0142385 159.1514 201.5572 14.46441776 02
| Epoch (UTC): | 17 April 2026 22:31:29 |
| Eccentricity: | 0.0142385 |
| inclination: | 96.4777° |
| perigee height: | 636 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 358.8658° |
| argument of perigee: | 159.1514° |
| revolutions per day: | 14.46441776 |
| mean anomaly at epoch: | 201.5572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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