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 23340.74788273 .00002238 00000-0 30649-3 0 9995
2 39766 97.9230 75.1711 0001468 101.2159 258.9217 14.79473505515070
| Epoch (UTC): | 06 December 2023 17:56:57 |
| Eccentricity: | 0.0001468 |
| inclination: | 97.9230° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 75.1711° |
| argument of perigee: | 101.2159° |
| revolutions per day: | 14.79473505 |
| mean anomaly at epoch: | 258.9217° |
| orbit number at epoch: | 51507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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