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 66890U 26145.58335647 +.00000000 +00000-0 +28608-2 0 00007
2 66890 53.1596 26.9269 0003570 81.4687 74.6266 15.34229197 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003570 |
| inclination: | 53.1596° |
| perigee height: | 461 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 26.9269° |
| argument of perigee: | 81.4687° |
| revolutions per day: | 15.34229197 |
| mean anomaly at epoch: | 74.6266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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