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 27422U 02021B 19345.79121984 -.00000025 +00000-0 +64647-5 0 9995
2 27422 098.3249 309.9551 0013372 070.2315 290.0309 14.29279342918217
Epoch (UTC): | 11 December 2019 18:59:21 |
Eccentricity: | 0.0013372 |
inclination: | 98.3249° |
perigee height: | 784 km |
apogee height: | 804 km |
right ascension of ascending node: | 309.9551° |
argument of perigee: | 70.2315° |
revolutions per day: | 14.29279342 |
mean anomaly at epoch: | 290.0309° |
orbit number at epoch: | 91821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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