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 66102U 26145.61770389 +.00000000 +00000-0 +47614-3 0 00002
2 66102 53.1593 106.4801 0001181 80.3929 279.7207 15.34413485 07
| Epoch (UTC): | 25 May 2026 14:49:29 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 106.4801° |
| argument of perigee: | 80.3929° |
| revolutions per day: | 15.34413485 |
| mean anomaly at epoch: | 279.7207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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