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 39026U 12072A 19051.16952364 .00001241 00000-0 47863-4 0 9994
2 39026 97.2109 58.1885 0039038 160.0852 200.1922 15.27466749343502
| Epoch (UTC): | 20 February 2019 04:04:06 |
| Eccentricity: | 0.0039038 |
| inclination: | 97.2109° |
| perigee height: | 456 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 58.1885° |
| argument of perigee: | 160.0852° |
| revolutions per day: | 15.27466749 |
| mean anomaly at epoch: | 200.1922° |
| orbit number at epoch: | 34350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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