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 22148.06697987 .00000389 00000-0 20987-3 0 9996
2 12 32.9082 27.7341 1665375 207.4208 142.7892 11.44669406603866
Epoch (UTC): | 28 May 2022 01:36:27 |
Eccentricity: | 0.1665375 |
inclination: | 32.9082° |
perigee height: | 553 km |
apogee height: | 3323 km |
right ascension of ascending node: | 27.7341° |
argument of perigee: | 207.4208° |
revolutions per day: | 11.44669406 |
mean anomaly at epoch: | 142.7892° |
orbit number at epoch: | 60386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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