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 26108.21710709 +.00000000 +00000-0 +28349-4 0 00003
2 25397 99.0060 99.4691 0002041 55.8767 304.2605 14.24416249 02
| Epoch (UTC): | 18 April 2026 05:12:38 |
| Eccentricity: | 0.0002041 |
| inclination: | 99.0060° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 99.4691° |
| argument of perigee: | 55.8767° |
| revolutions per day: | 14.24416249 |
| mean anomaly at epoch: | 304.2605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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