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 39446U 13066AG 19343.96645604 .00000148 00000-0 26351-4 0 9996
2 39446 97.5868 339.3905 0069202 210.3482 149.3716 14.78462117325015
Epoch (UTC): | 09 December 2019 23:11:41 |
Eccentricity: | 0.0069202 |
inclination: | 97.5868° |
perigee height: | 585 km |
apogee height: | 683 km |
right ascension of ascending node: | 339.3905° |
argument of perigee: | 210.3482° |
revolutions per day: | 14.78462117 |
mean anomaly at epoch: | 149.3716° |
orbit number at epoch: | 32501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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