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 29079U 06014A 19047.82835369 .00001627 00000-0 71184-4 0 9994
2 29079 97.4057 168.0930 0003018 171.2711 305.2170 15.23484839711149
Epoch (UTC): | 16 February 2019 19:52:49 |
Eccentricity: | 0.0003018 |
inclination: | 97.4057° |
perigee height: | 493 km |
apogee height: | 497 km |
right ascension of ascending node: | 168.0930° |
argument of perigee: | 171.2711° |
revolutions per day: | 15.23484839 |
mean anomaly at epoch: | 305.2170° |
orbit number at epoch: | 71114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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