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 22220U 92076B 24317.47637928 .00000022 00000-0 35000-4 0 9991
2 22220 70.9980 124.0631 0010615 114.3347 276.5762 14.16734597653866
Epoch (UTC): | 12 November 2024 11:25:59 |
Eccentricity: | 0.0010615 |
inclination: | 70.9980° |
perigee height: | 829 km |
apogee height: | 844 km |
right ascension of ascending node: | 124.0631° |
argument of perigee: | 114.3347° |
revolutions per day: | 14.16734597 |
mean anomaly at epoch: | 276.5762° |
orbit number at epoch: | 65386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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