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 40071U 14037C 24252.15849840 .00006843 00000-0 79740-3 0 9992
2 40071 98.3271 168.4249 0006979 203.2871 156.8027 14.85565230549952
Epoch (UTC): | 08 September 2024 03:48:14 |
Eccentricity: | 0.0006979 |
inclination: | 98.3271° |
perigee height: | 607 km |
apogee height: | 616 km |
right ascension of ascending node: | 168.4249° |
argument of perigee: | 203.2871° |
revolutions per day: | 14.85565230 |
mean anomaly at epoch: | 156.8027° |
orbit number at epoch: | 54995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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