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 44248U 19029P 19344.25002315 -.00019233 00000-0 -10890-2 0 9992
2 44248 52.9991 352.3833 0001467 73.9559 258.7203 15.12134780 30251
Epoch (UTC): | 10 December 2019 06:00:02 |
Eccentricity: | 0.0001467 |
inclination: | 52.9991° |
perigee height: | 528 km |
apogee height: | 531 km |
right ascension of ascending node: | 352.3833° |
argument of perigee: | 73.9559° |
revolutions per day: | 15.12134780 |
mean anomaly at epoch: | 258.7203° |
orbit number at epoch: | 3025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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