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 22144.85664541 .00000193 00000-0 93661-4 0 9991
2 24277 98.9338 147.1216 0002231 102.7568 257.3862 14.29536922343751
Epoch (UTC): | 24 May 2022 20:33:34 |
Eccentricity: | 0.0002231 |
inclination: | 98.9338° |
perigee height: | 791 km |
apogee height: | 795 km |
right ascension of ascending node: | 147.1216° |
argument of perigee: | 102.7568° |
revolutions per day: | 14.29536922 |
mean anomaly at epoch: | 257.3862° |
orbit number at epoch: | 34375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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