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 22143.19508839 .00000211 00000-0 99834-3 0 9996
2 27518 28.8356 34.3782 7132149 126.3653 321.9123 2.36569099170106
| Epoch (UTC): | 23 May 2022 04:40:55 |
| Eccentricity: | 0.7132149 |
| inclination: | 28.8356° |
| perigee height: | 445 km |
| apogee height: | 34382 km |
| right ascension of ascending node: | 34.3782° |
| argument of perigee: | 126.3653° |
| revolutions per day: | 2.36569099 |
| mean anomaly at epoch: | 321.9123° |
| orbit number at epoch: | 17010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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