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 47068U 93036BXY 24276.36161174 .00014104 00000-0 38314-2 0 9997
2 47068 74.0258 304.5706 0017152 140.4357 219.8058 14.47479559554280
Epoch (UTC): | 02 October 2024 08:40:43 |
Eccentricity: | 0.0017152 |
inclination: | 74.0258° |
perigee height: | 721 km |
apogee height: | 746 km |
right ascension of ascending node: | 304.5706° |
argument of perigee: | 140.4357° |
revolutions per day: | 14.47479559 |
mean anomaly at epoch: | 219.8058° |
orbit number at epoch: | 55428 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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