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 66290U 26145.39565135 +.00000000 +00000-0 +74058-3 0 00008
2 66290 53.1600 194.0167 0001062 66.8452 293.2663 15.34402344 09
| Epoch (UTC): | 25 May 2026 09:29:44 |
| Eccentricity: | 0.0001062 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 194.0167° |
| argument of perigee: | 66.8452° |
| revolutions per day: | 15.34402344 |
| mean anomaly at epoch: | 293.2663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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