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 66146U 26145.47243925 +.00000000 +00000-0 +48962-3 0 00002
2 66146 53.1584 65.5033 0001089 93.8612 266.2516 15.34408177 08
| Epoch (UTC): | 25 May 2026 11:20:18 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 65.5033° |
| argument of perigee: | 93.8612° |
| revolutions per day: | 15.34408177 |
| mean anomaly at epoch: | 266.2516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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