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 21799U 91076C 23269.11421075 0.00004700 00000-0 53032-3 0 04
2 21799 63.3109 272.2398 0900548 56.7957 303.2043 13.45567407 07
Epoch (UTC): | 26 September 2023 02:44:27 |
Eccentricity: | 0.0900548 |
inclination: | 63.3109° |
perigee height: | 416 km |
apogee height: | 1761 km |
right ascension of ascending node: | 272.2398° |
argument of perigee: | 56.7957° |
revolutions per day: | 13.45567407 |
mean anomaly at epoch: | 303.2043° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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