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 37839U 11058B 24340.46384656 .00000841 00000-0 30110-3 0 9991
2 37839 19.9601 102.1110 0018822 27.2599 30.9439 14.13441469679871
Epoch (UTC): | 05 December 2024 11:07:56 |
Eccentricity: | 0.0018822 |
inclination: | 19.9601° |
perigee height: | 834 km |
apogee height: | 861 km |
right ascension of ascending node: | 102.1110° |
argument of perigee: | 27.2599° |
revolutions per day: | 14.13441469 |
mean anomaly at epoch: | 30.9439° |
orbit number at epoch: | 67987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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