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 5U 58002B 22147.48548478 .00000344 00000-0 41752-3 0 9997
2 5 34.2539 204.0425 1847336 303.1171 40.5233 10.84951467282350
Epoch (UTC): | 27 May 2022 11:39:05 |
Eccentricity: | 0.1847336 |
inclination: | 34.2539° |
perigee height: | 649 km |
apogee height: | 3833 km |
right ascension of ascending node: | 204.0425° |
argument of perigee: | 303.1171° |
revolutions per day: | 10.84951467 |
mean anomaly at epoch: | 40.5233° |
orbit number at epoch: | 28235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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