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 32785U 08021C 23340.89855653 .00004039 00000-0 38262-3 0 9997
2 32785 97.7296 303.5728 0009986 247.3381 112.6783 14.94130812846666
| Epoch (UTC): | 06 December 2023 21:33:55 |
| Eccentricity: | 0.0009986 |
| inclination: | 97.7296° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 303.5728° |
| argument of perigee: | 247.3381° |
| revolutions per day: | 14.94130812 |
| mean anomaly at epoch: | 112.6783° |
| orbit number at epoch: | 84666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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