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 66509U 26145.64501052 +.00000000 +00000-0 +58143-3 0 00004
2 66509 42.9976 276.4878 0000785 251.1236 108.9530 15.27594015 02
| Epoch (UTC): | 25 May 2026 15:28:48 |
| Eccentricity: | 0.0000785 |
| inclination: | 42.9976° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.4878° |
| argument of perigee: | 251.1236° |
| revolutions per day: | 15.27594015 |
| mean anomaly at epoch: | 108.9530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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