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 26066.80949197 +.00000000 +00000-0 +81184-4 0 00003
2 25893 82.9306 172.8394 0028786 183.7568 292.7507 13.76826828 03
| Epoch (UTC): | 07 March 2026 19:25:40 |
| Eccentricity: | 0.0028786 |
| inclination: | 82.9306° |
| perigee height: | 954 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 172.8394° |
| argument of perigee: | 183.7568° |
| revolutions per day: | 13.76826828 |
| mean anomaly at epoch: | 292.7507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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