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 25893U 26065.55282834 +.00000000 +00000-0 +68616-4 0 00007
2 25893 82.9305 173.7746 0028699 187.3437 183.9302 13.76826551 08
| Epoch (UTC): | 06 March 2026 13:16:04 |
| Eccentricity: | 0.0028699 |
| inclination: | 82.9305° |
| perigee height: | 954 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 173.7746° |
| argument of perigee: | 187.3437° |
| revolutions per day: | 13.76826551 |
| mean anomaly at epoch: | 183.9302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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