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 65977U 26145.50436507 +.00000000 +00000-0 -49473-2 0 00005
2 65977 81.3002 232.9777 0001342 99.1236 261.0071 13.81492540 01
| Epoch (UTC): | 25 May 2026 12:06:17 |
| Eccentricity: | 0.0001342 |
| inclination: | 81.3002° |
| perigee height: | 958 km |
| apogee height: | 960 km |
| right ascension of ascending node: | 232.9777° |
| argument of perigee: | 99.1236° |
| revolutions per day: | 13.81492540 |
| mean anomaly at epoch: | 261.0071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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