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 66222U 26145.53612064 +.00000000 +00000-0 +46966-3 0 00000
2 66222 53.1581 233.0661 0000647 305.9900 54.1041 15.30201478 03
| Epoch (UTC): | 25 May 2026 12:52:00 |
| Eccentricity: | 0.0000647 |
| inclination: | 53.1581° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.0661° |
| argument of perigee: | 305.9900° |
| revolutions per day: | 15.30201478 |
| mean anomaly at epoch: | 54.1041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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