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 12U 59001B 23029.01857914 .00001460 00000-0 88188-3 0 9996
2 12 32.8946 246.6036 1661110 61.4149 314.3474 11.44923909632060
Epoch (UTC): | 29 January 2023 00:26:45 |
Eccentricity: | 0.1661110 |
inclination: | 32.8946° |
perigee height: | 556 km |
apogee height: | 3318 km |
right ascension of ascending node: | 246.6036° |
argument of perigee: | 61.4149° |
revolutions per day: | 11.44923909 |
mean anomaly at epoch: | 314.3474° |
orbit number at epoch: | 63206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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