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 18265.95501472 +.00000118 +00000-0 +16886-4 0 9999
2 42849 097.5868 165.5058 0006923 224.5647 135.5016 14.92243099064927
| Epoch (UTC): | 22 September 2018 22:55:13 |
| Eccentricity: | 0.0006923 |
| inclination: | 97.5868° |
| perigee height: | 586 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 165.5058° |
| argument of perigee: | 224.5647° |
| revolutions per day: | 14.92243099 |
| mean anomaly at epoch: | 135.5016° |
| orbit number at epoch: | 6492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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