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 20203U 89069B 23079.50255431 .00000034 00000-0 00000-0 0 9992
2 20203 14.2566 12.7097 0012395 9.8284 200.5641 0.99117757 13244
Epoch (UTC): | 20 March 2023 12:03:40 |
Eccentricity: | 0.0012395 |
inclination: | 14.2566° |
perigee height: | 36060 km |
apogee height: | 36165 km |
right ascension of ascending node: | 12.7097° |
argument of perigee: | 9.8284° |
revolutions per day: | 0.99117757 |
mean anomaly at epoch: | 200.5641° |
orbit number at epoch: | 1324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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