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 65985U 26145.53992404 +.00000000 +00000-0 +10290-3 0 00005
2 65985 81.2986 232.6938 0002623 194.8966 165.2114 13.84758009 03
| Epoch (UTC): | 25 May 2026 12:57:29 |
| Eccentricity: | 0.0002623 |
| inclination: | 81.2986° |
| perigee height: | 945 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 232.6938° |
| argument of perigee: | 194.8966° |
| revolutions per day: | 13.84758009 |
| mean anomaly at epoch: | 165.2114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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