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 23156.35693673 .00000034 00000-0 42802-4 0 9994
2 23087 71.0533 124.0148 0007094 139.1828 220.9827 14.13966779502250
Epoch (UTC): | 05 June 2023 08:33:59 |
Eccentricity: | 0.0007094 |
inclination: | 71.0533° |
perigee height: | 841 km |
apogee height: | 851 km |
right ascension of ascending node: | 124.0148° |
argument of perigee: | 139.1828° |
revolutions per day: | 14.13966779 |
mean anomaly at epoch: | 220.9827° |
orbit number at epoch: | 50225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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