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 32268U 07049A 19005.18753767 .99999999 32729-5 85228-3 0 9998
2 32268 61.7933 196.9521 0719552 252.7837 233.5623 15.00311182 83229
| Epoch (UTC): | 05 January 2019 04:30:03 |
| Eccentricity: | 0.0719552 |
| inclination: | 61.7933° |
| perigee height: | 66 km |
| apogee height: | 1065 km |
| right ascension of ascending node: | 196.9521° |
| argument of perigee: | 252.7837° |
| revolutions per day: | 15.00311182 |
| mean anomaly at epoch: | 233.5623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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