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 36734U 99025EBG 24278.02259396 .00018816 00000-0 86479-2 0 9997
2 36734 99.0871 305.5094 0037570 29.2752 331.0518 14.20816412765406
Epoch (UTC): | 04 October 2024 00:32:32 |
Eccentricity: | 0.0037570 |
inclination: | 99.0871° |
perigee height: | 795 km |
apogee height: | 849 km |
right ascension of ascending node: | 305.5094° |
argument of perigee: | 29.2752° |
revolutions per day: | 14.20816412 |
mean anomaly at epoch: | 331.0518° |
orbit number at epoch: | 76540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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