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 data is extracted from the following two-line orbital elements,
1 36122U 09072B 23273.88101159 -.00000040 00000-0 96979-5 0 9992
2 36122 100.2518 234.4762 0007414 345.5566 14.5334 13.16387966662803
| Epoch (UTC): | 30 September 2023 21:08:39 |
| Eccentricity: | 0.0007414 |
| inclination: | 100.2518° |
| perigee height: | 1193 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 234.4762° |
| argument of perigee: | 345.5566° |
| revolutions per day: | 13.16387966 |
| mean anomaly at epoch: | 14.5334° |
| orbit number at epoch: | 66280 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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