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 31792U 07029A 24282.20649590 .00001377 00000-0 76673-3 0 9993
2 31792 70.9359 209.5599 0009939 255.1799 104.8221 14.12751798891005
Epoch (UTC): | 08 October 2024 04:57:21 |
Eccentricity: | 0.0009939 |
inclination: | 70.9359° |
perigee height: | 843 km |
apogee height: | 857 km |
right ascension of ascending node: | 209.5599° |
argument of perigee: | 255.1799° |
revolutions per day: | 14.12751798 |
mean anomaly at epoch: | 104.8221° |
orbit number at epoch: | 89100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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