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 43131U 18004W 22178.18667142 .00019900 00000-0 55650-3 0 9993
2 43131 97.3761 257.4892 0004512 317.3698 42.7196 15.36697865248079
Epoch (UTC): | 27 June 2022 04:28:48 |
Eccentricity: | 0.0004512 |
inclination: | 97.3761° |
perigee height: | 453 km |
apogee height: | 459 km |
right ascension of ascending node: | 257.4892° |
argument of perigee: | 317.3698° |
revolutions per day: | 15.36697865 |
mean anomaly at epoch: | 42.7196° |
orbit number at epoch: | 24807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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