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 20U 59007A 19342.86903166 +.00000012 +00000-0 -45275-6 0 9994
2 20 033.3464 144.5637 1667186 330.4394 021.1262 11.55690732208438
Epoch (UTC): | 08 December 2019 20:51:24 |
Eccentricity: | 0.1667186 |
inclination: | 33.3464° |
perigee height: | 508 km |
apogee height: | 3263 km |
right ascension of ascending node: | 144.5637° |
argument of perigee: | 330.4394° |
revolutions per day: | 11.55690732 |
mean anomaly at epoch: | 21.1262° |
orbit number at epoch: | 20843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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