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 is defined by the following mean orbital elements,
1 41120U 11077AK 19210.76630294 -.00000492 00000-0 -56385-1 0 9999
2 41120 26.8759 353.7873 7318689 272.0230 13.9514 1.88905713 29748
| Epoch (UTC): | 29 July 2019 18:23:28 |
| Eccentricity: | 0.7318689 |
| inclination: | 26.8759° |
| perigee height: | 1033 km |
| apogee height: | 41494 km |
| right ascension of ascending node: | 353.7873° |
| argument of perigee: | 272.0230° |
| revolutions per day: | 1.88905713 |
| mean anomaly at epoch: | 13.9514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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