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 00016U 58002A 24313.86655539 .00000563 00000-0 76772-3 0 9998
2 00016 34.2606 197.7891 2023329 168.7786 196.5889 10.49479074627417
Epoch (UTC): | 08 November 2024 20:47:50 |
Eccentricity: | 0.2023329 |
inclination: | 34.2606° |
perigee height: | 651 km |
apogee height: | 4217 km |
right ascension of ascending node: | 197.7891° |
argument of perigee: | 168.7786° |
revolutions per day: | 10.49479074 |
mean anomaly at epoch: | 196.5889° |
orbit number at epoch: | 62741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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