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 66292U 26145.58474748 +.00000000 +00000-0 +30246-3 0 00001
2 66292 53.1590 193.0644 0001184 79.3163 280.7973 15.34395219 08
| Epoch (UTC): | 25 May 2026 14:02:02 |
| Eccentricity: | 0.0001184 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 193.0644° |
| argument of perigee: | 79.3163° |
| revolutions per day: | 15.34395219 |
| mean anomaly at epoch: | 280.7973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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