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 65679U 26144.99869429 +.00000000 +00000-0 +85042-3 0 00001
2 65679 53.1591 351.4516 0000886 86.3856 273.7246 15.30206668 00
| Epoch (UTC): | 24 May 2026 23:58:07 |
| Eccentricity: | 0.0000886 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.4516° |
| argument of perigee: | 86.3856° |
| revolutions per day: | 15.30206668 |
| mean anomaly at epoch: | 273.7246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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