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 33591U 09005A 22179.82384524 .00000120 00000-0 89801-4 0 9995
2 33591 99.1467 214.1992 0014447 152.5622 207.6315 14.12581799690051
Epoch (UTC): | 28 June 2022 19:46:20 |
Eccentricity: | 0.0014447 |
inclination: | 99.1467° |
perigee height: | 840 km |
apogee height: | 861 km |
right ascension of ascending node: | 214.1992° |
argument of perigee: | 152.5622° |
revolutions per day: | 14.12581799 |
mean anomaly at epoch: | 207.6315° |
orbit number at epoch: | 69005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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