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 39841U 92093KT 22147.81342050 .00015192 00000-0 14902-2 0 9993
2 39841 70.7526 343.0751 0037975 120.9677 252.1829 14.91744023432115
Epoch (UTC): | 27 May 2022 19:31:19 |
Eccentricity: | 0.0037975 |
inclination: | 70.7526° |
perigee height: | 566 km |
apogee height: | 619 km |
right ascension of ascending node: | 343.0751° |
argument of perigee: | 120.9677° |
revolutions per day: | 14.91744023 |
mean anomaly at epoch: | 252.1829° |
orbit number at epoch: | 43211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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