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 66853U 26145.36120541 +.00000000 +00000-0 +85351-3 0 00006
2 66853 42.9936 270.2859 0000486 321.1845 38.8971 15.27595646 04
| Epoch (UTC): | 25 May 2026 08:40:08 |
| Eccentricity: | 0.0000486 |
| inclination: | 42.9936° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 270.2859° |
| argument of perigee: | 321.1845° |
| revolutions per day: | 15.27595646 |
| mean anomaly at epoch: | 38.8971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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