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 39770U 14029E 24224.87032687 .18403858 29146-5 12830-2 0 9997
2 39770 97.9775 25.0334 0015086 283.9081 76.0538 16.39772937556368
Epoch (UTC): | 11 August 2024 20:53:16 |
Eccentricity: | 0.0015086 |
inclination: | 97.9775° |
perigee height: | 156 km |
apogee height: | 176 km |
right ascension of ascending node: | 25.0334° |
argument of perigee: | 283.9081° |
revolutions per day: | 16.39772937 |
mean anomaly at epoch: | 76.0538° |
orbit number at epoch: | 55636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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