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 23150.41441705 .00000217 00000-0 13885-3 0 9993
2 23087 71.0526 136.4389 0007540 149.2797 210.8769 14.13964547501410
Epoch (UTC): | 30 May 2023 09:56:45 |
Eccentricity: | 0.0007540 |
inclination: | 71.0526° |
perigee height: | 840 km |
apogee height: | 851 km |
right ascension of ascending node: | 136.4389° |
argument of perigee: | 149.2797° |
revolutions per day: | 14.13964547 |
mean anomaly at epoch: | 210.8769° |
orbit number at epoch: | 50141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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