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 23342.57396887 .00001860 00000-0 25584-3 0 9996
2 39766 97.9235 76.9715 0001431 99.5546 260.5827 14.79471569515318
| Epoch (UTC): | 08 December 2023 13:46:30 |
| Eccentricity: | 0.0001431 |
| inclination: | 97.9235° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 76.9715° |
| argument of perigee: | 99.5546° |
| revolutions per day: | 14.79471569 |
| mean anomaly at epoch: | 260.5827° |
| orbit number at epoch: | 51531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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