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 39770U 14029E 22178.11343388 .00005381 00000-0 54943-3 0 9998
2 39770 97.9439 295.1106 0009744 59.8621 300.3455 14.91001007439108
Epoch (UTC): | 27 June 2022 02:43:20 |
Eccentricity: | 0.0009744 |
inclination: | 97.9439° |
perigee height: | 588 km |
apogee height: | 601 km |
right ascension of ascending node: | 295.1106° |
argument of perigee: | 59.8621° |
revolutions per day: | 14.91001007 |
mean anomaly at epoch: | 300.3455° |
orbit number at epoch: | 43910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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