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 51U 60009C 22145.79829730 -.00000030 00000-0 53731-3 0 9996
2 51 47.2135 319.0724 0108433 106.1516 255.1238 12.18282701750319
Epoch (UTC): | 25 May 2022 19:09:32 |
Eccentricity: | 0.0108433 |
inclination: | 47.2135° |
perigee height: | 1513 km |
apogee height: | 1686 km |
right ascension of ascending node: | 319.0724° |
argument of perigee: | 106.1516° |
revolutions per day: | 12.18282701 |
mean anomaly at epoch: | 255.1238° |
orbit number at epoch: | 75031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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