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 66017U 26145.58335647 +.00000000 +00000-0 -12002-3 0 00001
2 66017 53.1598 106.7881 0001567 92.2390 54.6309 15.34389745 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001567 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 106.7881° |
| argument of perigee: | 92.2390° |
| revolutions per day: | 15.34389745 |
| mean anomaly at epoch: | 54.6309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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