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 40074U 14037F 19345.93772051 +.00000298 +00000-0 +42844-4 0 9991
2 40074 098.4490 158.1001 0005245 022.1557 337.9893 14.84153243293792
Epoch (UTC): | 11 December 2019 22:30:19 |
Eccentricity: | 0.0005245 |
inclination: | 98.4490° |
perigee height: | 612 km |
apogee height: | 620 km |
right ascension of ascending node: | 158.1001° |
argument of perigee: | 22.1557° |
revolutions per day: | 14.84153243 |
mean anomaly at epoch: | 337.9893° |
orbit number at epoch: | 29379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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