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 42849U 17042AA 19082.66849273 .00000264 00000-0 31062-4 0 9994
2 42849 97.5761 340.4659 0007952 356.8791 3.2377 14.92324250 92024
| Epoch (UTC): | 23 March 2019 16:02:37 |
| Eccentricity: | 0.0007952 |
| inclination: | 97.5761° |
| perigee height: | 585 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 340.4659° |
| argument of perigee: | 356.8791° |
| revolutions per day: | 14.92324250 |
| mean anomaly at epoch: | 3.2377° |
| orbit number at epoch: | 9202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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