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 33498U 09002G 21060.44551309 .00000249 00000-0 40915-4 0 9996
2 33498 98.2303 298.0938 0010462 340.3155 19.7650 14.79287428651492
Epoch (UTC): | 01 March 2021 10:41:32 |
Eccentricity: | 0.0010462 |
inclination: | 98.2303° |
perigee height: | 624 km |
apogee height: | 639 km |
right ascension of ascending node: | 298.0938° |
argument of perigee: | 340.3155° |
revolutions per day: | 14.79287428 |
mean anomaly at epoch: | 19.7650° |
orbit number at epoch: | 65149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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