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 23333.33407294 .00050759 00000-0 28650-2 0 9997
2 39770 98.0020 106.7881 0004420 126.1447 234.0192 15.12945465517021
Epoch (UTC): | 29 November 2023 08:01:03 |
Eccentricity: | 0.0004420 |
inclination: | 98.0020° |
perigee height: | 524 km |
apogee height: | 530 km |
right ascension of ascending node: | 106.7881° |
argument of perigee: | 126.1447° |
revolutions per day: | 15.12945465 |
mean anomaly at epoch: | 234.0192° |
orbit number at epoch: | 51702 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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