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 27733U 81053MN 24357.14181463 .00005563 00000-0 27274-2 0 9991
2 27733 83.1115 245.5568 0026126 197.7414 162.2857 14.17464754290441
Epoch (UTC): | 22 December 2024 03:24:12 |
Eccentricity: | 0.0026126 |
inclination: | 83.1115° |
perigee height: | 815 km |
apogee height: | 853 km |
right ascension of ascending node: | 245.5568° |
argument of perigee: | 197.7414° |
revolutions per day: | 14.17464754 |
mean anomaly at epoch: | 162.2857° |
orbit number at epoch: | 29044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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