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 41557U 16033B 22142.18656406 .00020293 00000-0 61534-3 0 9990
2 41557 97.3868 239.8529 0012950 113.2749 96.4510 15.34073660333354
Epoch (UTC): | 22 May 2022 04:28:39 |
Eccentricity: | 0.0012950 |
inclination: | 97.3868° |
perigee height: | 455 km |
apogee height: | 472 km |
right ascension of ascending node: | 239.8529° |
argument of perigee: | 113.2749° |
revolutions per day: | 15.34073660 |
mean anomaly at epoch: | 96.4510° |
orbit number at epoch: | 33335 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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