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 39287U 13056C 22138.13465678 .00000989 00000-0 33990-3 0 9993
2 39287 49.5430 68.2104 5196869 267.8490 34.6843 5.24672087163444
Epoch (UTC): | 18 May 2022 03:13:54 |
Eccentricity: | 0.5196869 |
inclination: | 49.5430° |
perigee height: | 341 km |
apogee height: | 14882 km |
right ascension of ascending node: | 68.2104° |
argument of perigee: | 267.8490° |
revolutions per day: | 5.24672087 |
mean anomaly at epoch: | 34.6843° |
orbit number at epoch: | 16344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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