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 20202U 89069A 23087.81924306 -.00000023 00000-0 00000-0 0 9997
2 20202 14.0649 344.7257 0014229 234.5601 305.8166 0.98610460 14203
Epoch (UTC): | 28 March 2023 19:39:42 |
Eccentricity: | 0.0014229 |
inclination: | 14.0649° |
perigee height: | 36198 km |
apogee height: | 36319 km |
right ascension of ascending node: | 344.7257° |
argument of perigee: | 234.5601° |
revolutions per day: | 0.98610460 |
mean anomaly at epoch: | 305.8166° |
orbit number at epoch: | 1420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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