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 66105U 26145.30351656 +.00000000 +00000-0 +91719-3 0 00008
2 66105 53.1584 108.0683 0001304 91.6427 268.4723 15.30207069 04
| Epoch (UTC): | 25 May 2026 07:17:03 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.0683° |
| argument of perigee: | 91.6427° |
| revolutions per day: | 15.30207069 |
| mean anomaly at epoch: | 268.4723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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