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 04139U 69091B 22227.88308246 .00000223 00000-0 49119-4 0 9991
2 04139 74.0314 88.7166 0004739 51.9536 308.2059 14.63282380804529
Epoch (UTC): | 15 August 2022 21:11:38 |
Eccentricity: | 0.0004739 |
inclination: | 74.0314° |
perigee height: | 679 km |
apogee height: | 686 km |
right ascension of ascending node: | 88.7166° |
argument of perigee: | 51.9536° |
revolutions per day: | 14.63282380 |
mean anomaly at epoch: | 308.2059° |
orbit number at epoch: | 80452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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