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 39087U 13009B 19047.80006222 .00000067 00000-0 38341-4 0 9997
2 39087 98.4953 256.0085 0011939 292.6400 67.3531 14.35695262312980
| Epoch (UTC): | 16 February 2019 19:12:05 |
| Eccentricity: | 0.0011939 |
| inclination: | 98.4953° |
| perigee height: | 764 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 256.0085° |
| argument of perigee: | 292.6400° |
| revolutions per day: | 14.35695262 |
| mean anomaly at epoch: | 67.3531° |
| orbit number at epoch: | 31298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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