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 40554U 15020C 23088.45303786 .00000011 00000-0 50058-5 0 9998
2 40554 82.4872 43.3163 0014383 22.2725 337.8983 12.42888500362729
Epoch (UTC): | 29 March 2023 10:52:22 |
Eccentricity: | 0.0014383 |
inclination: | 82.4872° |
perigee height: | 1483 km |
apogee height: | 1506 km |
right ascension of ascending node: | 43.3163° |
argument of perigee: | 22.2725° |
revolutions per day: | 12.42888500 |
mean anomaly at epoch: | 337.8983° |
orbit number at epoch: | 36272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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