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 42836U 17042M 19077.64113414 .00000168 00000-0 22319-4 0 9991
2 42836 97.5753 334.5161 0013703 15.2831 344.8799 14.91153240 91248
| Epoch (UTC): | 18 March 2019 15:23:13 |
| Eccentricity: | 0.0013703 |
| inclination: | 97.5753° |
| perigee height: | 585 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 334.5161° |
| argument of perigee: | 15.2831° |
| revolutions per day: | 14.91153240 |
| mean anomaly at epoch: | 344.8799° |
| orbit number at epoch: | 9124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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