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 26097.96153850 +.00000000 +00000-0 +57257-4 0 00000
2 25397 99.0054 88.9576 0002254 72.0602 288.0821 14.24414445 00
| Epoch (UTC): | 07 April 2026 23:04:36 |
| Eccentricity: | 0.0002254 |
| inclination: | 99.0054° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 88.9576° |
| argument of perigee: | 72.0602° |
| revolutions per day: | 14.24414445 |
| mean anomaly at epoch: | 288.0821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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