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 14085U 83048B 24282.48896215 .00000433 00000-0 42588-3 0 9992
2 14085 82.9393 267.5218 0032977 195.9198 164.0925 13.76500422 77703
Epoch (UTC): | 08 October 2024 11:44:06 |
Eccentricity: | 0.0032977 |
inclination: | 82.9393° |
perigee height: | 952 km |
apogee height: | 1000 km |
right ascension of ascending node: | 267.5218° |
argument of perigee: | 195.9198° |
revolutions per day: | 13.76500422 |
mean anomaly at epoch: | 164.0925° |
orbit number at epoch: | 7770 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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