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 66591U 26145.57398006 +.00000000 +00000-0 +48286-3 0 00007
2 66591 42.9990 342.0414 0000688 293.2182 66.8597 15.27592205 08
| Epoch (UTC): | 25 May 2026 13:46:31 |
| Eccentricity: | 0.0000688 |
| inclination: | 42.9990° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 342.0414° |
| argument of perigee: | 293.2182° |
| revolutions per day: | 15.27592205 |
| mean anomaly at epoch: | 66.8597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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