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 66237U 26145.41264058 +.00000000 +00000-0 +77383-3 0 00006
2 66237 53.1586 286.0728 0001424 80.2388 279.8775 15.34417061 04
| Epoch (UTC): | 25 May 2026 09:54:12 |
| Eccentricity: | 0.0001424 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 286.0728° |
| argument of perigee: | 80.2388° |
| revolutions per day: | 15.34417061 |
| mean anomaly at epoch: | 279.8775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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