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 39770U 14029E 23340.34281737 .00036164 00000-0 20061-2 0 9990
2 39770 98.0007 114.1434 0004345 95.7012 264.4714 15.13660565518088
| Epoch (UTC): | 06 December 2023 08:13:39 |
| Eccentricity: | 0.0004345 |
| inclination: | 98.0007° |
| perigee height: | 522 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 114.1434° |
| argument of perigee: | 95.7012° |
| revolutions per day: | 15.13660565 |
| mean anomaly at epoch: | 264.4714° |
| orbit number at epoch: | 51808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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