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 40564U 95015DX 23339.58847680 .00009856 00000-0 32114-2 0 9996
2 40564 98.6752 21.0339 0024558 97.0991 263.2989 14.38710332454302
Epoch (UTC): | 05 December 2023 14:07:24 |
Eccentricity: | 0.0024558 |
inclination: | 98.6752° |
perigee height: | 745 km |
apogee height: | 780 km |
right ascension of ascending node: | 21.0339° |
argument of perigee: | 97.0991° |
revolutions per day: | 14.38710332 |
mean anomaly at epoch: | 263.2989° |
orbit number at epoch: | 45430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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