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 39136U 13015G 22178.42081348 .00007638 00000-0 32978-3 0 9998
2 39136 64.8757 73.6697 0016877 295.8941 64.0447 15.23067917507431
Epoch (UTC): | 27 June 2022 10:05:58 |
Eccentricity: | 0.0016877 |
inclination: | 64.8757° |
perigee height: | 485 km |
apogee height: | 508 km |
right ascension of ascending node: | 73.6697° |
argument of perigee: | 295.8941° |
revolutions per day: | 15.23067917 |
mean anomaly at epoch: | 64.0447° |
orbit number at epoch: | 50743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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