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 43201U 18016A 18233.17438851 .08479562 -41201-5 49811-3 0 9991
2 43201 30.9356 166.7823 0085811 113.9593 247.7760 16.27471364 28751
| Epoch (UTC): | 21 August 2018 04:11:07 |
| Eccentricity: | 0.0085811 |
| inclination: | 30.9356° |
| perigee height: | 143 km |
| apogee height: | 256 km |
| right ascension of ascending node: | 166.7823° |
| argument of perigee: | 113.9593° |
| revolutions per day: | 16.27471364 |
| mean anomaly at epoch: | 247.7760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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