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 37818U 11052A 23333.87505827 .00011719 00000-0 38739-2 0 9993
2 37818 62.8624 31.8906 4698300 254.3720 50.6010 6.05598246268000
Epoch (UTC): | 29 November 2023 21:00:05 |
Eccentricity: | 0.4698300 |
inclination: | 62.8624° |
perigee height: | 362 km |
apogee height: | 12309 km |
right ascension of ascending node: | 31.8906° |
argument of perigee: | 254.3720° |
revolutions per day: | 6.05598246 |
mean anomaly at epoch: | 50.6010° |
orbit number at epoch: | 26800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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