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 670U 63038B 19341.51770041 .00000053 00000-0 75073-4 0 9990
2 670 90.0477 330.9388 0041923 18.8604 341.4085 13.44319570754505
Epoch (UTC): | 07 December 2019 12:25:29 |
Eccentricity: | 0.0041923 |
inclination: | 90.0477° |
perigee height: | 1062 km |
apogee height: | 1124 km |
right ascension of ascending node: | 330.9388° |
argument of perigee: | 18.8604° |
revolutions per day: | 13.44319570 |
mean anomaly at epoch: | 341.4085° |
orbit number at epoch: | 75450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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