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 40017U 14033H 24284.47252602 .00014395 00000-0 99345-3 0 9996
2 40017 98.1097 313.1904 0015968 138.0118 222.2335 15.05801073562305
Epoch (UTC): | 10 October 2024 11:20:26 |
Eccentricity: | 0.0015968 |
inclination: | 98.1097° |
perigee height: | 538 km |
apogee height: | 560 km |
right ascension of ascending node: | 313.1904° |
argument of perigee: | 138.0118° |
revolutions per day: | 15.05801073 |
mean anomaly at epoch: | 222.2335° |
orbit number at epoch: | 56230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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