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 20883U 90081AT 24357.91469903 .00003251 00000-0 11480-2 0 9998
2 20883 98.5651 348.0173 0012342 171.8677 244.9348 14.35337086772866
Epoch (UTC): | 22 December 2024 21:57:09 |
Eccentricity: | 0.0012342 |
inclination: | 98.5651° |
perigee height: | 765 km |
apogee height: | 783 km |
right ascension of ascending node: | 348.0173° |
argument of perigee: | 171.8677° |
revolutions per day: | 14.35337086 |
mean anomaly at epoch: | 244.9348° |
orbit number at epoch: | 77286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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