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 66966U 26145.15107344 +.00000000 +00000-0 +71986-3 0 00003
2 66966 42.9985 311.4272 0001289 270.9217 89.1487 15.27560990 01
| Epoch (UTC): | 25 May 2026 03:37:32 |
| Eccentricity: | 0.0001289 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 311.4272° |
| argument of perigee: | 270.9217° |
| revolutions per day: | 15.27560990 |
| mean anomaly at epoch: | 89.1487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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