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 25634U 99008A 24276.82725425 .00000661 00000-0 33181-3 0 9994
2 25634 98.4313 258.4625 0011124 49.7317 310.4831 14.19740871325981
Epoch (UTC): | 02 October 2024 19:51:14 |
Eccentricity: | 0.0011124 |
inclination: | 98.4313° |
perigee height: | 818 km |
apogee height: | 834 km |
right ascension of ascending node: | 258.4625° |
argument of perigee: | 49.7317° |
revolutions per day: | 14.19740871 |
mean anomaly at epoch: | 310.4831° |
orbit number at epoch: | 32598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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