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 43832U 18102B 22179.57731421 .00007695 00000-0 42422-3 0 9997
2 43832 97.5085 256.3502 0014969 133.9516 337.7504 15.14166801196048
Epoch (UTC): | 28 June 2022 13:51:19 |
Eccentricity: | 0.0014969 |
inclination: | 97.5085° |
perigee height: | 513 km |
apogee height: | 534 km |
right ascension of ascending node: | 256.3502° |
argument of perigee: | 133.9516° |
revolutions per day: | 15.14166801 |
mean anomaly at epoch: | 337.7504° |
orbit number at epoch: | 19604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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