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 38770U 12048N 22225.95574636 0.00004100 00000-0 22771-3 0 08
2 38770 64.6564 192.7597 0177501 249.3531 110.6469 15.00933639 02
Epoch (UTC): | 13 August 2022 22:56:16 |
Eccentricity: | 0.0177501 |
inclination: | 64.6564° |
perigee height: | 441 km |
apogee height: | 687 km |
right ascension of ascending node: | 192.7597° |
argument of perigee: | 249.3531° |
revolutions per day: | 15.00933639 |
mean anomaly at epoch: | 110.6469° |
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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