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 22179.25430973 .00004796 00000-0 49034-3 0 9995
2 39770 97.9435 296.2591 0009422 59.6126 300.5963 14.91007902439279
Epoch (UTC): | 28 June 2022 06:06:12 |
Eccentricity: | 0.0009422 |
inclination: | 97.9435° |
perigee height: | 588 km |
apogee height: | 601 km |
right ascension of ascending node: | 296.2591° |
argument of perigee: | 59.6126° |
revolutions per day: | 14.91007902 |
mean anomaly at epoch: | 300.5963° |
orbit number at epoch: | 43927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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