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 26141.21284907 +.00000000 +00000-0 +48118-4 0 00008
2 25636 96.4733 24.3299 0143263 54.3791 307.0654 14.46456371 09
| Epoch (UTC): | 21 May 2026 05:06:30 |
| Eccentricity: | 0.0143263 |
| inclination: | 96.4733° |
| perigee height: | 635 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 24.3299° |
| argument of perigee: | 54.3791° |
| revolutions per day: | 14.46456371 |
| mean anomaly at epoch: | 307.0654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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