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 20U 59007A 24314.09579859 .00003202 00000-0 12890-2 0 9998
2 20 33.3402 210.4652 1645669 161.3031 205.6056 11.60101125416622
Epoch (UTC): | 09 November 2024 02:17:56 |
Eccentricity: | 0.1645669 |
inclination: | 33.3402° |
perigee height: | 508 km |
apogee height: | 3221 km |
right ascension of ascending node: | 210.4652° |
argument of perigee: | 161.3031° |
revolutions per day: | 11.60101125 |
mean anomaly at epoch: | 205.6056° |
orbit number at epoch: | 41662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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