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 66583U 26145.65047169 +.00000000 +00000-0 +98269-3 0 00004
2 66583 42.9996 272.1003 0001428 273.7758 86.2931 15.27585949 02
| Epoch (UTC): | 25 May 2026 15:36:40 |
| Eccentricity: | 0.0001428 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.1003° |
| argument of perigee: | 273.7758° |
| revolutions per day: | 15.27585949 |
| mean anomaly at epoch: | 86.2931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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