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 43137U 18004AC 23091.17645560 .00048118 00000-0 11795-2 0 9997
2 43137 97.3339 169.8277 0006312 67.9470 292.2446 15.40559725290439
Epoch (UTC): | 01 April 2023 04:14:05 |
Eccentricity: | 0.0006312 |
inclination: | 97.3339° |
perigee height: | 440 km |
apogee height: | 449 km |
right ascension of ascending node: | 169.8277° |
argument of perigee: | 67.9470° |
revolutions per day: | 15.40559725 |
mean anomaly at epoch: | 292.2446° |
orbit number at epoch: | 29043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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