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 23156.86958323 -.00000016 00000-0 -32862-4 0 9999
2 23604 82.9026 335.0213 0022904 292.1475 67.7250 13.74353072400172
Epoch (UTC): | 05 June 2023 20:52:11 |
Eccentricity: | 0.0022904 |
inclination: | 82.9026° |
perigee height: | 967 km |
apogee height: | 1001 km |
right ascension of ascending node: | 335.0213° |
argument of perigee: | 292.1475° |
revolutions per day: | 13.74353072 |
mean anomaly at epoch: | 67.7250° |
orbit number at epoch: | 40017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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