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 24298U 96051B 24311.85443105 .00000026 00000-0 40366-4 0 9998
2 24298 70.7868 127.3280 0013944 138.9676 221.2495 14.12456693452767
Epoch (UTC): | 06 November 2024 20:30:22 |
Eccentricity: | 0.0013944 |
inclination: | 70.7868° |
perigee height: | 841 km |
apogee height: | 861 km |
right ascension of ascending node: | 127.3280° |
argument of perigee: | 138.9676° |
revolutions per day: | 14.12456693 |
mean anomaly at epoch: | 221.2495° |
orbit number at epoch: | 45276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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