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 23604U 95032B 23150.02616107 -.00000010 00000-0 -26359-4 0 9990
2 23604 82.9028 340.1145 0023157 312.2295 47.6895 13.74353506399463
Epoch (UTC): | 30 May 2023 00:37:40 |
Eccentricity: | 0.0023157 |
inclination: | 82.9028° |
perigee height: | 967 km |
apogee height: | 1001 km |
right ascension of ascending node: | 340.1145° |
argument of perigee: | 312.2295° |
revolutions per day: | 13.74353506 |
mean anomaly at epoch: | 47.6895° |
orbit number at epoch: | 39946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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