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 25160U 26145.66700293 +.00000000 +00000-0 +75407-4 0 00005
2 25160 108.0113 286.8511 0061871 173.2112 198.2902 14.22477783 07
| Epoch (UTC): | 25 May 2026 16:00:29 |
| Eccentricity: | 0.0061871 |
| inclination: | 108.0113° |
| perigee height: | 772 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 286.8511° |
| argument of perigee: | 173.2112° |
| revolutions per day: | 14.22477783 |
| mean anomaly at epoch: | 198.2902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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