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 24317.00579877 .00000493 00000-0 66575-3 0 9990
2 00016 34.2614 188.7081 2023396 182.0427 177.0634 10.49482384627748
Epoch (UTC): | 12 November 2024 00:08:21 |
Eccentricity: | 0.2023396 |
inclination: | 34.2614° |
perigee height: | 651 km |
apogee height: | 4217 km |
right ascension of ascending node: | 188.7081° |
argument of perigee: | 182.0427° |
revolutions per day: | 10.49482384 |
mean anomaly at epoch: | 177.0634° |
orbit number at epoch: | 62774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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