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 66979U 26145.45888359 +.00000000 +00000-0 +53294-3 0 00004
2 66979 43.0012 310.2957 0001525 265.6949 94.3728 15.27595517 00
| Epoch (UTC): | 25 May 2026 11:00:47 |
| Eccentricity: | 0.0001525 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 310.2957° |
| argument of perigee: | 265.6949° |
| revolutions per day: | 15.27595517 |
| mean anomaly at epoch: | 94.3728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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