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 26071.54984197 +.00000000 +00000-0 +73993-4 0 00007
2 25397 99.0029 61.8925 0002134 115.0247 245.1152 14.24407055 00
| Epoch (UTC): | 12 March 2026 13:11:46 |
| Eccentricity: | 0.0002134 |
| inclination: | 99.0029° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 61.8925° |
| argument of perigee: | 115.0247° |
| revolutions per day: | 14.24407055 |
| mean anomaly at epoch: | 245.1152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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