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 66563U 26145.40563469 +.00000000 +00000-0 +68035-3 0 00009
2 66563 43.0016 273.7141 0000556 280.1424 79.9365 15.27593086 09
| Epoch (UTC): | 25 May 2026 09:44:06 |
| Eccentricity: | 0.0000556 |
| inclination: | 43.0016° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 273.7141° |
| argument of perigee: | 280.1424° |
| revolutions per day: | 15.27593086 |
| mean anomaly at epoch: | 79.9365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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