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 38770U 12048N 24286.26483756 .00040750 00000-0 14511-2 0 9993
2 38770 64.6482 172.4069 0104491 340.8174 18.9030 15.23624899 23951
Epoch (UTC): | 12 October 2024 06:21:21 |
Eccentricity: | 0.0104491 |
inclination: | 64.6482° |
perigee height: | 423 km |
apogee height: | 567 km |
right ascension of ascending node: | 172.4069° |
argument of perigee: | 340.8174° |
revolutions per day: | 15.23624899 |
mean anomaly at epoch: | 18.9030° |
orbit number at epoch: | 2395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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