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 10537U 77122B 22177.15227559 .00000086 00000-0 73834-4 0 9993
2 10537 82.9331 195.3409 0018595 302.9946 123.2849 13.75286759233309
Epoch (UTC): | 26 June 2022 03:39:16 |
Eccentricity: | 0.0018595 |
inclination: | 82.9331° |
perigee height: | 967 km |
apogee height: | 994 km |
right ascension of ascending node: | 195.3409° |
argument of perigee: | 302.9946° |
revolutions per day: | 13.75286759 |
mean anomaly at epoch: | 123.2849° |
orbit number at epoch: | 23330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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