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 66160U 26145.16536940 +.00000000 +00000-0 +64181-3 0 00007
2 66160 53.1596 67.8463 0000859 109.2970 250.8124 15.30212946 09
| Epoch (UTC): | 25 May 2026 03:58:07 |
| Eccentricity: | 0.0000859 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 67.8463° |
| argument of perigee: | 109.2970° |
| revolutions per day: | 15.30212946 |
| mean anomaly at epoch: | 250.8124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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