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 66083U 26145.28447701 +.00000000 +00000-0 +66960-3 0 00007
2 66083 53.1598 249.8294 0001563 93.7938 266.3241 15.30209104 07
| Epoch (UTC): | 25 May 2026 06:49:38 |
| Eccentricity: | 0.0001563 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 249.8294° |
| argument of perigee: | 93.7938° |
| revolutions per day: | 15.30209104 |
| mean anomaly at epoch: | 266.3241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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