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 39061U 13002A 22227.02520062 0.00000000 00000-0 00000-0 0 00
2 39061 97.5121 347.3921 0002513 241.6374 118.3625 15.17601585 08
Epoch (UTC): | 15 August 2022 00:36:17 |
Eccentricity: | 0.0002513 |
inclination: | 97.5121° |
perigee height: | 511 km |
apogee height: | 515 km |
right ascension of ascending node: | 347.3921° |
argument of perigee: | 241.6374° |
revolutions per day: | 15.17601585 |
mean anomaly at epoch: | 118.3625° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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