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 36105U 09066B 21044.17338895 0.00001000 00000-0 52377-4 0 03
2 36105 97.2869 41.1565 0030197 16.2159 343.7839 15.15449457 06
Epoch (UTC): | 13 February 2021 04:09:40 |
Eccentricity: | 0.0030197 |
inclination: | 97.2869° |
perigee height: | 499 km |
apogee height: | 540 km |
right ascension of ascending node: | 41.1565° |
argument of perigee: | 16.2159° |
revolutions per day: | 15.15449457 |
mean anomaly at epoch: | 343.7839° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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