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 38736U 12041D 23088.25506552 .00000026 00000-0 11561-3 0 9991
2 38736 82.4753 85.5011 0026281 101.4914 258.9114 12.43843311484182
Epoch (UTC): | 29 March 2023 06:07:17 |
Eccentricity: | 0.0026281 |
inclination: | 82.4753° |
perigee height: | 1469 km |
apogee height: | 1511 km |
right ascension of ascending node: | 85.5011° |
argument of perigee: | 101.4914° |
revolutions per day: | 12.43843311 |
mean anomaly at epoch: | 258.9114° |
orbit number at epoch: | 48418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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