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 24277U 96046A 22139.74720646 .00000259 00000-0 11974-3 0 9991
2 24277 98.9341 141.8823 0002211 110.9113 249.2305 14.29534642343024
Epoch (UTC): | 19 May 2022 17:55:58 |
Eccentricity: | 0.0002211 |
inclination: | 98.9341° |
perigee height: | 792 km |
apogee height: | 795 km |
right ascension of ascending node: | 141.8823° |
argument of perigee: | 110.9113° |
revolutions per day: | 14.29534642 |
mean anomaly at epoch: | 249.2305° |
orbit number at epoch: | 34302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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