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 65980U 26145.52266014 +.00000000 +00000-0 +34558-4 0 00004
2 65980 81.2998 232.9902 0001062 123.2435 236.8821 13.80999012 05
| Epoch (UTC): | 25 May 2026 12:32:37 |
| Eccentricity: | 0.0001062 |
| inclination: | 81.2998° |
| perigee height: | 960 km |
| apogee height: | 961 km |
| right ascension of ascending node: | 232.9902° |
| argument of perigee: | 123.2435° |
| revolutions per day: | 13.80999012 |
| mean anomaly at epoch: | 236.8821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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