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 4564U 70079A 22229.44686778 -.00000072 00000-0 13299-4 0 9997
2 4564 65.2796 13.0377 0074673 252.8659 106.4214 13.78456090610773
Epoch (UTC): | 17 August 2022 10:43:29 |
Eccentricity: | 0.0074673 |
inclination: | 65.2796° |
perigee height: | 914 km |
apogee height: | 1024 km |
right ascension of ascending node: | 13.0377° |
argument of perigee: | 252.8659° |
revolutions per day: | 13.78456090 |
mean anomaly at epoch: | 106.4214° |
orbit number at epoch: | 61077 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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