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 22287U 92094B 22144.20771210 .00000359 00000-0 46064-4 0 9999
2 22287 82.5258 201.1770 0024416 190.0227 170.0502 14.78280736584759
Epoch (UTC): | 24 May 2022 04:59:06 |
Eccentricity: | 0.0024416 |
inclination: | 82.5258° |
perigee height: | 617 km |
apogee height: | 652 km |
right ascension of ascending node: | 201.1770° |
argument of perigee: | 190.0227° |
revolutions per day: | 14.78280736 |
mean anomaly at epoch: | 170.0502° |
orbit number at epoch: | 58475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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