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 33061U 08031B 24357.66717045 .00004026 00000-0 56026-3 0 9996
2 33061 48.4435 82.8656 0005152 332.1052 176.6842 14.79513706888086
Epoch (UTC): | 22 December 2024 16:00:43 |
Eccentricity: | 0.0005152 |
inclination: | 48.4435° |
perigee height: | 627 km |
apogee height: | 634 km |
right ascension of ascending node: | 82.8656° |
argument of perigee: | 332.1052° |
revolutions per day: | 14.79513706 |
mean anomaly at epoch: | 176.6842° |
orbit number at epoch: | 88808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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