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 26073.26441553 +.00000000 +00000-0 +62311-4 0 00005
2 25893 82.9304 168.0354 0029204 165.8977 246.8875 13.76827855 04
| Epoch (UTC): | 14 March 2026 06:20:45 |
| Eccentricity: | 0.0029204 |
| inclination: | 82.9304° |
| perigee height: | 954 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 168.0354° |
| argument of perigee: | 165.8977° |
| revolutions per day: | 13.76827855 |
| mean anomaly at epoch: | 246.8875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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