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 66520U 26145.46941936 +.00000000 +00000-0 +48900-3 0 00006
2 66520 43.0005 204.5246 0001326 260.5059 99.5643 15.27577359 02
| Epoch (UTC): | 25 May 2026 11:15:57 |
| Eccentricity: | 0.0001326 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.5246° |
| argument of perigee: | 260.5059° |
| revolutions per day: | 15.27577359 |
| mean anomaly at epoch: | 99.5643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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