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 27424U 02022A 18203.63526622 +.00000054 +00000-0 +22131-4 0 9993
2 27424 098.2037 144.3004 0001736 009.7420 342.7416 14.57079242862537
| Epoch (UTC): | 22 July 2018 15:14:47 |
| Eccentricity: | 0.0001736 |
| inclination: | 98.2037° |
| perigee height: | 701 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 144.3004° |
| argument of perigee: | 9.7420° |
| revolutions per day: | 14.57079242 |
| mean anomaly at epoch: | 342.7416° |
| orbit number at epoch: | 86253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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