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 66239U 26145.42519826 +.00000000 +00000-0 +25416-3 0 00005
2 66239 53.1583 287.5692 0000403 307.8856 52.2109 15.30205440 09
| Epoch (UTC): | 25 May 2026 10:12:17 |
| Eccentricity: | 0.0000403 |
| inclination: | 53.1583° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 287.5692° |
| argument of perigee: | 307.8856° |
| revolutions per day: | 15.30205440 |
| mean anomaly at epoch: | 52.2109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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