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 43261U 18031C 22183.79515220 .00000921 00000-0 13429-3 0 9990
2 43261 97.9125 262.3781 0002497 315.5447 44.5563 14.78148536229479
Epoch (UTC): | 02 July 2022 19:05:01 |
Eccentricity: | 0.0002497 |
inclination: | 97.9125° |
perigee height: | 633 km |
apogee height: | 637 km |
right ascension of ascending node: | 262.3781° |
argument of perigee: | 315.5447° |
revolutions per day: | 14.78148536 |
mean anomaly at epoch: | 44.5563° |
orbit number at epoch: | 22947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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