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 66807U 26145.40771823 +.00000000 +00000-0 +13322-2 0 00003
2 66807 43.0003 40.9790 0001404 273.6149 86.4542 15.27605141 00
| Epoch (UTC): | 25 May 2026 09:47:06 |
| Eccentricity: | 0.0001404 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.9790° |
| argument of perigee: | 273.6149° |
| revolutions per day: | 15.27605141 |
| mean anomaly at epoch: | 86.4542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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