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 23223U 94054A 20086.43965028 0.00000000 00000-0 00000-0 0 00
2 23223 11.8511 25.9770 0026338 126.5847 233.6283 1.00270000 03
Epoch (UTC): | 26 March 2020 10:33:05 |
Eccentricity: | 0.0026338 |
inclination: | 11.8511° |
perigee height: | 35675 km |
apogee height: | 35898 km |
right ascension of ascending node: | 25.9770° |
argument of perigee: | 126.5847° |
revolutions per day: | 1.00270000 |
mean anomaly at epoch: | 233.6283° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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