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 66479U 26145.60167966 +.00000000 +00000-0 +31688-3 0 00003
2 66479 43.0030 221.4172 0001821 277.1326 82.9319 15.27585451 08
| Epoch (UTC): | 25 May 2026 14:26:25 |
| Eccentricity: | 0.0001821 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.4172° |
| argument of perigee: | 277.1326° |
| revolutions per day: | 15.27585451 |
| mean anomaly at epoch: | 82.9319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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