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 11765U 80030A 22144.86212263 .00002642 00000-0 12904-3 0 9997
2 11765 66.0876 33.2006 0547914 298.7301 55.9785 14.41668643163810
Epoch (UTC): | 24 May 2022 20:41:27 |
Eccentricity: | 0.0547914 |
inclination: | 66.0876° |
perigee height: | 362 km |
apogee height: | 1144 km |
right ascension of ascending node: | 33.2006° |
argument of perigee: | 298.7301° |
revolutions per day: | 14.41668643 |
mean anomaly at epoch: | 55.9785° |
orbit number at epoch: | 16381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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