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 22176.75407436 .00017839 00000-0 50025-3 0 9992
2 43131 97.3760 256.0526 0004588 324.2638 35.8298 15.36633930247855
Epoch (UTC): | 25 June 2022 18:05:52 |
Eccentricity: | 0.0004588 |
inclination: | 97.3760° |
perigee height: | 453 km |
apogee height: | 459 km |
right ascension of ascending node: | 256.0526° |
argument of perigee: | 324.2638° |
revolutions per day: | 15.36633930 |
mean anomaly at epoch: | 35.8298° |
orbit number at epoch: | 24785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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