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 11U 59001A 22221.55374636 .00000128 00000-0 64664-4 0 9996
2 11 32.8730 354.4944 1466526 353.4950 4.8357 11.86160060709708
Epoch (UTC): | 09 August 2022 13:17:23 |
Eccentricity: | 0.1466526 |
inclination: | 32.8730° |
perigee height: | 552 km |
apogee height: | 2934 km |
right ascension of ascending node: | 354.4944° |
argument of perigee: | 353.4950° |
revolutions per day: | 11.86160060 |
mean anomaly at epoch: | 4.8357° |
orbit number at epoch: | 70970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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