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 40039U 14033AF 23083.49258135 .00004642 00000-0 51516-3 0 9997
2 40039 97.8931 6.5702 0012383 234.8785 125.1271 14.87675984475137
Epoch (UTC): | 24 March 2023 11:49:19 |
Eccentricity: | 0.0012383 |
inclination: | 97.8931° |
perigee height: | 596 km |
apogee height: | 614 km |
right ascension of ascending node: | 6.5702° |
argument of perigee: | 234.8785° |
revolutions per day: | 14.87675984 |
mean anomaly at epoch: | 125.1271° |
orbit number at epoch: | 47513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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