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 66011U 26145.33507804 +.00000000 +00000-0 +30258-3 0 00006
2 66011 53.1583 107.6622 0001302 92.6687 267.4463 15.30204124 03
| Epoch (UTC): | 25 May 2026 08:02:30 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 107.6622° |
| argument of perigee: | 92.6687° |
| revolutions per day: | 15.30204124 |
| mean anomaly at epoch: | 267.4463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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