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 18322.92881817 +.00000073 +00000-0 +26260-4 0 9995
2 27424 098.2103 261.7851 0001663 009.9831 061.7094 14.57109251879916
| Epoch (UTC): | 18 November 2018 22:17:29 |
| Eccentricity: | 0.0001663 |
| inclination: | 98.2103° |
| perigee height: | 701 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 261.7851° |
| argument of perigee: | 9.9831° |
| revolutions per day: | 14.57109251 |
| mean anomaly at epoch: | 61.7094° |
| orbit number at epoch: | 87991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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