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 10061U 77048A 19345.49037323 .00000045 00000-0 00000+0 0 9995
2 10061 11.7805 317.2567 0017299 350.4988 25.1564 0.99393094 99869
Epoch (UTC): | 11 December 2019 11:46:08 |
Eccentricity: | 0.0017299 |
inclination: | 11.7805° |
perigee height: | 35961 km |
apogee height: | 36108 km |
right ascension of ascending node: | 317.2567° |
argument of perigee: | 350.4988° |
revolutions per day: | 0.99393094 |
mean anomaly at epoch: | 25.1564° |
orbit number at epoch: | 9986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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