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 23088.88615052 .00061538 00000-0 10950-2 0 9991
2 41557 97.3823 194.2265 0007333 77.4429 62.7328 15.49917780381308
Epoch (UTC): | 29 March 2023 21:16:03 |
Eccentricity: | 0.0007333 |
inclination: | 97.3823° |
perigee height: | 412 km |
apogee height: | 422 km |
right ascension of ascending node: | 194.2265° |
argument of perigee: | 77.4429° |
revolutions per day: | 15.49917780 |
mean anomaly at epoch: | 62.7328° |
orbit number at epoch: | 38130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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