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 19345.72249524 +.00000169 +00000-0 +30434-4 0 9999
2 33498 098.2854 200.4198 0010351 330.1760 029.8859 14.79062774585601
Epoch (UTC): | 11 December 2019 17:20:23 |
Eccentricity: | 0.0010351 |
inclination: | 98.2854° |
perigee height: | 625 km |
apogee height: | 639 km |
right ascension of ascending node: | 200.4198° |
argument of perigee: | 330.1760° |
revolutions per day: | 14.79062774 |
mean anomaly at epoch: | 29.8859° |
orbit number at epoch: | 58560 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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