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 39172U 13026A 19049.49216007 -.00000278 00000-0 00000+0 0 9993
2 39172 0.0715 292.6609 0002248 26.7532 325.3882 1.00271942 20887
| Epoch (UTC): | 18 February 2019 11:48:42 |
| Eccentricity: | 0.0002248 |
| inclination: | 0.0715° |
| perigee height: | 35776 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 292.6609° |
| argument of perigee: | 26.7532° |
| revolutions per day: | 1.00271942 |
| mean anomaly at epoch: | 325.3882° |
| orbit number at epoch: | 2088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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