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 66792U 26145.40001076 +.00000000 +00000-0 +81969-3 0 00005
2 66792 43.0002 40.9156 0000841 279.4630 80.6127 15.27591807 09
| Epoch (UTC): | 25 May 2026 09:36:00 |
| Eccentricity: | 0.0000841 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.9156° |
| argument of perigee: | 279.4630° |
| revolutions per day: | 15.27591807 |
| mean anomaly at epoch: | 80.6127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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