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 04159U 69082AB 21018.60703509 -.00000029 00000-0 22093-4 0 9998
2 04159 69.9636 336.6139 0118620 258.3724 100.4036 13.72454034567577
Epoch (UTC): | 18 January 2021 14:34:07 |
Eccentricity: | 0.0118620 |
inclination: | 69.9636° |
perigee height: | 903 km |
apogee height: | 1078 km |
right ascension of ascending node: | 336.6139° |
argument of perigee: | 258.3724° |
revolutions per day: | 13.72454034 |
mean anomaly at epoch: | 100.4036° |
orbit number at epoch: | 56757 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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