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 66978U 26145.47287966 +.00000000 +00000-0 +56942-3 0 00005
2 66978 43.0008 309.5467 0001205 265.9928 94.0786 15.27577972 02
| Epoch (UTC): | 25 May 2026 11:20:56 |
| Eccentricity: | 0.0001205 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.5467° |
| argument of perigee: | 265.9928° |
| revolutions per day: | 15.27577972 |
| mean anomaly at epoch: | 94.0786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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