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 39765U 14028E 19047.75204825 .00000039 00000-0 10000-3 0 9995
2 39765 82.4404 259.9069 0231258 167.0916 193.6247 12.82920908221924
| Epoch (UTC): | 16 February 2019 18:02:56 |
| Eccentricity: | 0.0231258 |
| inclination: | 82.4404° |
| perigee height: | 1151 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 259.9069° |
| argument of perigee: | 167.0916° |
| revolutions per day: | 12.82920908 |
| mean anomaly at epoch: | 193.6247° |
| orbit number at epoch: | 22192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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