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 66519U 26145.52581010 +.00000000 +00000-0 +72004-3 0 00006
2 66519 43.0010 204.0807 0001415 282.6891 77.3803 15.27587721 08
| Epoch (UTC): | 25 May 2026 12:37:09 |
| Eccentricity: | 0.0001415 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.0807° |
| argument of perigee: | 282.6891° |
| revolutions per day: | 15.27587721 |
| mean anomaly at epoch: | 77.3803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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