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 00020U 59007A 24311.85839914 .00003225 00000-0 13009-2 0 9998
2 00020 33.3397 218.4983 1645719 149.3418 221.4655 11.60086799416339
Epoch (UTC): | 06 November 2024 20:36:05 |
Eccentricity: | 0.1645719 |
inclination: | 33.3397° |
perigee height: | 508 km |
apogee height: | 3221 km |
right ascension of ascending node: | 218.4983° |
argument of perigee: | 149.3418° |
revolutions per day: | 11.60086799 |
mean anomaly at epoch: | 221.4655° |
orbit number at epoch: | 41633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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