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 27598U 02056B 21023.59194751 -.00000004 00000-0 15633-4 0 9990
2 27598 98.6010 329.4877 0008816 344.3214 15.7693 14.28726994944292
Epoch (UTC): | 23 January 2021 14:12:24 |
Eccentricity: | 0.0008816 |
inclination: | 98.6010° |
perigee height: | 789 km |
apogee height: | 802 km |
right ascension of ascending node: | 329.4877° |
argument of perigee: | 344.3214° |
revolutions per day: | 14.28726994 |
mean anomaly at epoch: | 15.7693° |
orbit number at epoch: | 94429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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