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 41704U 10007W 24191.70386788 -.00001195 00000-0 -29034-1 0 9995
2 41704 65.1010 97.7847 5402330 307.8265 14.5457 4.35437325149197
Epoch (UTC): | 09 July 2024 16:53:34 |
Eccentricity: | 0.5402330 |
inclination: | 65.1010° |
perigee height: | 905 km |
apogee height: | 18020 km |
right ascension of ascending node: | 97.7847° |
argument of perigee: | 307.8265° |
revolutions per day: | 4.35437325 |
mean anomaly at epoch: | 14.5457° |
orbit number at epoch: | 14919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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