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 66969U 26145.45502865 +.00000000 +00000-0 +11159-2 0 00001
2 66969 43.0017 310.2756 0001219 241.8567 118.2162 15.27596796 01
| Epoch (UTC): | 25 May 2026 10:55:14 |
| Eccentricity: | 0.0001219 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 310.2756° |
| argument of perigee: | 241.8567° |
| revolutions per day: | 15.27596796 |
| mean anomaly at epoch: | 118.2162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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