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 66435U 26145.44029407 +.00000000 +00000-0 +51976-3 0 00006
2 66435 43.0017 200.5225 0001155 250.3912 109.6815 15.27589788 01
| Epoch (UTC): | 25 May 2026 10:34:01 |
| Eccentricity: | 0.0001155 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.5225° |
| argument of perigee: | 250.3912° |
| revolutions per day: | 15.27589788 |
| mean anomaly at epoch: | 109.6815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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