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 28352U 04021A 22227.80910401 .00000326 00000-0 20493-3 0 9997
2 28352 71.0026 147.1378 0011519 136.0348 224.1691 14.11730401936916
Epoch (UTC): | 15 August 2022 19:25:06 |
Eccentricity: | 0.0011519 |
inclination: | 71.0026° |
perigee height: | 845 km |
apogee height: | 862 km |
right ascension of ascending node: | 147.1378° |
argument of perigee: | 136.0348° |
revolutions per day: | 14.11730401 |
mean anomaly at epoch: | 224.1691° |
orbit number at epoch: | 93691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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