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 66946U 26145.57912852 +.00000000 +00000-0 +63061-3 0 00000
2 66946 53.1608 0.9668 0001207 88.8086 271.3055 15.34407228 02
| Epoch (UTC): | 25 May 2026 13:53:56 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1608° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 0.9668° |
| argument of perigee: | 88.8086° |
| revolutions per day: | 15.34407228 |
| mean anomaly at epoch: | 271.3055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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