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 25157U 26140.60121485 +.00000000 +00000-0 +57628-3 0 00004
2 25157 108.0082 90.6527 0031225 39.2783 321.0689 15.78241916 08
| Epoch (UTC): | 20 May 2026 14:25:44 |
| Eccentricity: | 0.0031225 |
| inclination: | 108.0082° |
| perigee height: | 314 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 90.6527° |
| argument of perigee: | 39.2783° |
| revolutions per day: | 15.78241916 |
| mean anomaly at epoch: | 321.0689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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