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 23092.23286935 .00070915 00000-0 12389-2 0 9996
2 41557 97.3827 197.6547 0006961 65.4346 19.2288 15.50403230381824
Epoch (UTC): | 02 April 2023 05:35:19 |
Eccentricity: | 0.0006961 |
inclination: | 97.3827° |
perigee height: | 411 km |
apogee height: | 420 km |
right ascension of ascending node: | 197.6547° |
argument of perigee: | 65.4346° |
revolutions per day: | 15.50403230 |
mean anomaly at epoch: | 19.2288° |
orbit number at epoch: | 38182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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