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 23153.10270085 .00000140 00000-0 98538-4 0 9997
2 23087 71.0531 130.8186 0007335 144.7539 215.4069 14.13965912502046
Epoch (UTC): | 02 June 2023 02:27:53 |
Eccentricity: | 0.0007335 |
inclination: | 71.0531° |
perigee height: | 840 km |
apogee height: | 851 km |
right ascension of ascending node: | 130.8186° |
argument of perigee: | 144.7539° |
revolutions per day: | 14.13965912 |
mean anomaly at epoch: | 215.4069° |
orbit number at epoch: | 50204 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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