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 24306.86657724 .00003498 00000-0 14147-2 0 9996
2 00020 33.3408 236.4162 1646066 122.6559 254.3614 11.60050753415753
Epoch (UTC): | 01 November 2024 20:47:52 |
Eccentricity: | 0.1646066 |
inclination: | 33.3408° |
perigee height: | 508 km |
apogee height: | 3221 km |
right ascension of ascending node: | 236.4162° |
argument of perigee: | 122.6559° |
revolutions per day: | 11.60050753 |
mean anomaly at epoch: | 254.3614° |
orbit number at epoch: | 41575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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