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 42761U 17034D 24277.21416370 .00046949 00000-0 13600-2 0 9995
2 42761 43.0209 331.7963 0012286 5.9718 354.1281 15.34769118403973
Epoch (UTC): | 03 October 2024 05:08:23 |
Eccentricity: | 0.0012286 |
inclination: | 43.0209° |
perigee height: | 453 km |
apogee height: | 470 km |
right ascension of ascending node: | 331.7963° |
argument of perigee: | 5.9718° |
revolutions per day: | 15.34769118 |
mean anomaly at epoch: | 354.1281° |
orbit number at epoch: | 40397 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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