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 42347U 00055QP 24285.22290724 .00220596 00000-0 68502-1 0 9995
2 42347 98.9488 76.3732 0042926 156.1558 204.1629 14.38933180453703
Epoch (UTC): | 11 October 2024 05:20:59 |
Eccentricity: | 0.0042926 |
inclination: | 98.9488° |
perigee height: | 731 km |
apogee height: | 792 km |
right ascension of ascending node: | 76.3732° |
argument of perigee: | 156.1558° |
revolutions per day: | 14.38933180 |
mean anomaly at epoch: | 204.1629° |
orbit number at epoch: | 45370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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