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 00107U 61013A 21110.55045592 .00000441 00000-0 41176-4 0 9991
2 00107 28.7872 246.8061 0545986 28.4671 334.4631 14.09177277 9587
Epoch (UTC): | 20 April 2021 13:12:39 |
Eccentricity: | 0.0545986 |
inclination: | 28.7872° |
perigee height: | 467 km |
apogee height: | 1257 km |
right ascension of ascending node: | 246.8061° |
argument of perigee: | 28.4671° |
revolutions per day: | 14.09177277 |
mean anomaly at epoch: | 334.4631° |
orbit number at epoch: | 958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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