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 20797U 90081G 24357.91350767 .00001948 00000-0 99076-3 0 9998
2 20797 98.7545 339.1702 0007620 243.3322 179.8887 14.16990922765283
Epoch (UTC): | 22 December 2024 21:55:27 |
Eccentricity: | 0.0007620 |
inclination: | 98.7545° |
perigee height: | 830 km |
apogee height: | 841 km |
right ascension of ascending node: | 339.1702° |
argument of perigee: | 243.3322° |
revolutions per day: | 14.16990922 |
mean anomaly at epoch: | 179.8887° |
orbit number at epoch: | 76528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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