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 22178.43241447 .00008043 00000-0 28306-3 0 9997
2 43137 97.3690 253.4992 0006479 337.5020 22.5936 15.29573231247877
Epoch (UTC): | 27 June 2022 10:22:40 |
Eccentricity: | 0.0006479 |
inclination: | 97.3690° |
perigee height: | 472 km |
apogee height: | 481 km |
right ascension of ascending node: | 253.4992° |
argument of perigee: | 337.5020° |
revolutions per day: | 15.29573231 |
mean anomaly at epoch: | 22.5936° |
orbit number at epoch: | 24787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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