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 24305U 96052B 19340.69932637 +.00000010 +00000-0 -56039-5 0 9998
2 24305 082.9387 044.7991 0031138 052.4749 307.9229 13.73815771165438
Epoch (UTC): | 06 December 2019 16:47:01 |
Eccentricity: | 0.0031138 |
inclination: | 82.9387° |
perigee height: | 963 km |
apogee height: | 1009 km |
right ascension of ascending node: | 44.7991° |
argument of perigee: | 52.4749° |
revolutions per day: | 13.73815771 |
mean anomaly at epoch: | 307.9229° |
orbit number at epoch: | 16543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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