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 23153.38567797 .00000129 00000-0 92820-4 0 9991
2 23087 71.0531 130.2268 0007316 144.3538 215.8074 14.13965991501838
Epoch (UTC): | 02 June 2023 09:15:22 |
Eccentricity: | 0.0007316 |
inclination: | 71.0531° |
perigee height: | 840 km |
apogee height: | 851 km |
right ascension of ascending node: | 130.2268° |
argument of perigee: | 144.3538° |
revolutions per day: | 14.13965991 |
mean anomaly at epoch: | 215.8074° |
orbit number at epoch: | 50183 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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