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 23090.68758744 .00065783 00000-0 11596-2 0 9991
2 41557 97.3817 196.0706 0007288 66.6348 39.3071 15.50166327381580
Epoch (UTC): | 31 March 2023 16:30:07 |
Eccentricity: | 0.0007288 |
inclination: | 97.3817° |
perigee height: | 411 km |
apogee height: | 421 km |
right ascension of ascending node: | 196.0706° |
argument of perigee: | 66.6348° |
revolutions per day: | 15.50166327 |
mean anomaly at epoch: | 39.3071° |
orbit number at epoch: | 38158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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