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 37852U 11061C 22183.85752009 .00004404 00000-0 19523-3 0 9991
2 37852 101.7151 317.9246 0142953 5.6905 354.5895 15.13966351583807
Epoch (UTC): | 02 July 2022 20:34:49 |
Eccentricity: | 0.0142953 |
inclination: | 101.7151° |
perigee height: | 425 km |
apogee height: | 623 km |
right ascension of ascending node: | 317.9246° |
argument of perigee: | 5.6905° |
revolutions per day: | 15.13966351 |
mean anomaly at epoch: | 354.5895° |
orbit number at epoch: | 58380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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