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 22135.92702012 .00013327 00000-0 58310-3 0 9994
2 39136 64.8753 211.8218 0014279 295.3155 64.6494 15.22230820500961
Epoch (UTC): | 15 May 2022 22:14:54 |
Eccentricity: | 0.0014279 |
inclination: | 64.8753° |
perigee height: | 489 km |
apogee height: | 509 km |
right ascension of ascending node: | 211.8218° |
argument of perigee: | 295.3155° |
revolutions per day: | 15.22230820 |
mean anomaly at epoch: | 64.6494° |
orbit number at epoch: | 50096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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