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 23028.69794861 .00097534 00000-0 13745-2 0 9990
2 43131 97.3504 115.5296 0005627 267.7578 92.3032 15.56272773281312
Epoch (UTC): | 28 January 2023 16:45:02 |
Eccentricity: | 0.0005627 |
inclination: | 97.3504° |
perigee height: | 394 km |
apogee height: | 402 km |
right ascension of ascending node: | 115.5296° |
argument of perigee: | 267.7578° |
revolutions per day: | 15.56272773 |
mean anomaly at epoch: | 92.3032° |
orbit number at epoch: | 28131 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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