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 66240U 26145.39670637 +.00000000 +00000-0 +66222-3 0 00001
2 66240 53.1599 287.3856 0001483 129.1826 230.9307 15.30210424 02
| Epoch (UTC): | 25 May 2026 09:31:15 |
| Eccentricity: | 0.0001483 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.3856° |
| argument of perigee: | 129.1826° |
| revolutions per day: | 15.30210424 |
| mean anomaly at epoch: | 230.9307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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