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 42737U 98067MS 18087.11387049 .13966215 12356-4 93055-3 0 9999
2 42737 51.6095 27.8979 0006293 234.7874 125.2564 16.40626348 47903
| Epoch (UTC): | 28 March 2018 02:43:58 |
| Eccentricity: | 0.0006293 |
| inclination: | 51.6095° |
| perigee height: | 160 km |
| apogee height: | 168 km |
| right ascension of ascending node: | 27.8979° |
| argument of perigee: | 234.7874° |
| revolutions per day: | 16.40626348 |
| mean anomaly at epoch: | 125.2564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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