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 39134U 13015E 22176.87213992 .00010199 00000-0 36435-3 0 9993
2 39134 64.8627 34.2591 0034937 278.3757 81.3414 15.28717719508523
Epoch (UTC): | 25 June 2022 20:55:52 |
Eccentricity: | 0.0034937 |
inclination: | 64.8627° |
perigee height: | 455 km |
apogee height: | 503 km |
right ascension of ascending node: | 34.2591° |
argument of perigee: | 278.3757° |
revolutions per day: | 15.28717719 |
mean anomaly at epoch: | 81.3414° |
orbit number at epoch: | 50852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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