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 27518U 02042D 22139.81566455 .00000064 00000-0 62069-3 0 9994
2 27518 28.8304 35.6070 7131936 124.3847 323.8592 2.36567676170097
| Epoch (UTC): | 19 May 2022 19:34:33 |
| Eccentricity: | 0.7131936 |
| inclination: | 28.8304° |
| perigee height: | 445 km |
| apogee height: | 34382 km |
| right ascension of ascending node: | 35.6070° |
| argument of perigee: | 124.3847° |
| revolutions per day: | 2.36567676 |
| mean anomaly at epoch: | 323.8592° |
| orbit number at epoch: | 17009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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