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 66279U 26145.39330882 +.00000000 +00000-0 +23053-3 0 00003
2 66279 53.1589 195.4222 0001083 86.9260 273.1865 15.30183880 00
| Epoch (UTC): | 25 May 2026 09:26:21 |
| Eccentricity: | 0.0001083 |
| inclination: | 53.1589° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 195.4222° |
| argument of perigee: | 86.9260° |
| revolutions per day: | 15.30183880 |
| mean anomaly at epoch: | 273.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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