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 42263U 95015GD 24274.09895340 .00005623 00000-0 38809-2 0 9990
2 42263 98.7762 143.6969 0119413 320.3813 38.8669 13.96168986480835
Epoch (UTC): | 30 September 2024 02:22:29 |
Eccentricity: | 0.0119413 |
inclination: | 98.7762° |
perigee height: | 820 km |
apogee height: | 994 km |
right ascension of ascending node: | 143.6969° |
argument of perigee: | 320.3813° |
revolutions per day: | 13.96168986 |
mean anomaly at epoch: | 38.8669° |
orbit number at epoch: | 48083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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