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 23087U 94023A 23151.90004794 .00000174 00000-0 11664-3 0 9996
2 23087 71.0529 133.3330 0007419 146.8015 213.3575 14.13965333501626
Epoch (UTC): | 31 May 2023 21:36:04 |
Eccentricity: | 0.0007419 |
inclination: | 71.0529° |
perigee height: | 840 km |
apogee height: | 851 km |
right ascension of ascending node: | 133.3330° |
argument of perigee: | 146.8015° |
revolutions per day: | 14.13965333 |
mean anomaly at epoch: | 213.3575° |
orbit number at epoch: | 50162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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