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 27006U 01056F 21103.17558420 -.00000051 00000-0 -67557-5 0 9999
2 27006 99.5112 236.9060 0013800 285.5038 129.3393 13.70964117967789
Epoch (UTC): | 13 April 2021 04:12:50 |
Eccentricity: | 0.0013800 |
inclination: | 99.5112° |
perigee height: | 986 km |
apogee height: | 1006 km |
right ascension of ascending node: | 236.9060° |
argument of perigee: | 285.5038° |
revolutions per day: | 13.70964117 |
mean anomaly at epoch: | 129.3393° |
orbit number at epoch: | 96778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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