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 26066.20799377 +.00000000 +00000-0 +76224-4 0 00009
2 25893 82.9305 173.2870 0028747 185.4147 191.4041 13.76826711 04
| Epoch (UTC): | 07 March 2026 04:59:30 |
| Eccentricity: | 0.0028747 |
| inclination: | 82.9305° |
| perigee height: | 954 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 173.2870° |
| argument of perigee: | 185.4147° |
| revolutions per day: | 13.76826711 |
| mean anomaly at epoch: | 191.4041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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