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 65981U 26145.36941878 +.00000000 +00000-0 -16977-1 0 00008
2 65981 81.3011 232.8505 0000658 259.4711 100.6371 13.83091840 03
| Epoch (UTC): | 25 May 2026 08:51:57 |
| Eccentricity: | 0.0000658 |
| inclination: | 81.3011° |
| perigee height: | 952 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 232.8505° |
| argument of perigee: | 259.4711° |
| revolutions per day: | 13.83091840 |
| mean anomaly at epoch: | 100.6371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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