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 22229.44714341 .00008594 00000-0 29498-3 0 9997
2 43137 97.3649 304.0854 0008690 137.9802 222.2106 15.30350595255671
Epoch (UTC): | 17 August 2022 10:43:53 |
Eccentricity: | 0.0008690 |
inclination: | 97.3649° |
perigee height: | 469 km |
apogee height: | 481 km |
right ascension of ascending node: | 304.0854° |
argument of perigee: | 137.9802° |
revolutions per day: | 15.30350595 |
mean anomaly at epoch: | 222.2106° |
orbit number at epoch: | 25567 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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