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 36273U 99025DXA 24352.78189150 .00001303 00000-0 65676-3 0 9991
2 36273 99.6432 187.1505 0096983 270.1390 88.8669 14.15953116611380
Epoch (UTC): | 17 December 2024 18:45:55 |
Eccentricity: | 0.0096983 |
inclination: | 99.6432° |
perigee height: | 769 km |
apogee height: | 909 km |
right ascension of ascending node: | 187.1505° |
argument of perigee: | 270.1390° |
revolutions per day: | 14.15953116 |
mean anomaly at epoch: | 88.8669° |
orbit number at epoch: | 61138 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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