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 39766U 14029A 23336.48700584 .00004919 00000-0 66494-3 0 9995
2 39766 97.9230 70.9713 0001336 100.2577 259.8786 14.79482323514418
| Epoch (UTC): | 02 December 2023 11:41:17 |
| Eccentricity: | 0.0001336 |
| inclination: | 97.9230° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 70.9713° |
| argument of perigee: | 100.2577° |
| revolutions per day: | 14.79482323 |
| mean anomaly at epoch: | 259.8786° |
| orbit number at epoch: | 51441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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