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 41733U 16051C 16232.51887598 .01476011 25927-5 88484-5 0 9993
2 41733 97.3458 148.9302 0007426 267.7603 175.4520 16.54555299 604
| Epoch (UTC): | 19 August 2016 12:27:10 |
| Eccentricity: | 0.0007426 |
| inclination: | 97.3458° |
| perigee height: | 122 km |
| apogee height: | 132 km |
| right ascension of ascending node: | 148.9302° |
| argument of perigee: | 267.7603° |
| revolutions per day: | 16.54555299 |
| mean anomaly at epoch: | 175.4520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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