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 20442U 90005G 24280.75380355 .00001063 00000-0 39978-3 0 9997
2 20442 98.8922 274.0147 0010939 214.4678 145.5797 14.33692087813767
Epoch (UTC): | 06 October 2024 18:05:28 |
Eccentricity: | 0.0010939 |
inclination: | 98.8922° |
perigee height: | 771 km |
apogee height: | 787 km |
right ascension of ascending node: | 274.0147° |
argument of perigee: | 214.4678° |
revolutions per day: | 14.33692087 |
mean anomaly at epoch: | 145.5797° |
orbit number at epoch: | 81376 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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