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 26070.80658028 +.00000000 +00000-0 +66100-4 0 00009
2 25893 82.9306 169.8646 0029038 172.7510 304.4538 13.76827481 06
| Epoch (UTC): | 11 March 2026 19:21:28 |
| Eccentricity: | 0.0029038 |
| inclination: | 82.9306° |
| perigee height: | 954 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 169.8646° |
| argument of perigee: | 172.7510° |
| revolutions per day: | 13.76827481 |
| mean anomaly at epoch: | 304.4538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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