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 25397U 26108.91954286 +.00000000 +00000-0 +31059-4 0 00002
2 25397 99.0060 100.1891 0002024 54.9019 305.2348 14.24416378 03
| Epoch (UTC): | 18 April 2026 22:04:08 |
| Eccentricity: | 0.0002024 |
| inclination: | 99.0060° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 100.1891° |
| argument of perigee: | 54.9019° |
| revolutions per day: | 14.24416378 |
| mean anomaly at epoch: | 305.2348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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