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 23339.19990445 .00142566 00000-0 10727-2 0 9995
2 43137 97.3069 62.4491 0003332 235.6762 124.4186 15.72106074328891
Epoch (UTC): | 05 December 2023 04:47:51 |
Eccentricity: | 0.0003332 |
inclination: | 97.3069° |
perigee height: | 350 km |
apogee height: | 355 km |
right ascension of ascending node: | 62.4491° |
argument of perigee: | 235.6762° |
revolutions per day: | 15.72106074 |
mean anomaly at epoch: | 124.4186° |
orbit number at epoch: | 32889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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