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 66808U 26145.05893418 +.00000000 +00000-0 +16652-3 0 00000
2 66808 42.9983 42.6491 0001403 273.8525 86.2166 15.27569060 01
| Epoch (UTC): | 25 May 2026 01:24:51 |
| Eccentricity: | 0.0001403 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 42.6491° |
| argument of perigee: | 273.8525° |
| revolutions per day: | 15.27569060 |
| mean anomaly at epoch: | 86.2166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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