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 23092.20643334 .01685058 19302-2 24986-2 0 9997
2 43131 97.3189 182.2641 0010084 281.2104 78.8044 16.05301885291286
Epoch (UTC): | 02 April 2023 04:57:15 |
Eccentricity: | 0.0010084 |
inclination: | 97.3189° |
perigee height: | 253 km |
apogee height: | 266 km |
right ascension of ascending node: | 182.2641° |
argument of perigee: | 281.2104° |
revolutions per day: | 16.05301885 |
mean anomaly at epoch: | 78.8044° |
orbit number at epoch: | 29128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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