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 66986U 26145.49728640 +.00000000 +00000-0 +67416-3 0 00003
2 66986 43.0016 309.7213 0000972 277.7127 82.3614 15.27594779 07
| Epoch (UTC): | 25 May 2026 11:56:05 |
| Eccentricity: | 0.0000972 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.7213° |
| argument of perigee: | 277.7127° |
| revolutions per day: | 15.27594779 |
| mean anomaly at epoch: | 82.3614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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