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 24792U 97020A 17328.50355308 .99999999 -17679-5 36908-3 0 9999
2 24792 86.3363 249.3166 0025759 119.9357 245.3296 16.58206397 76471
| Epoch (UTC): | 24 November 2017 12:05:06 |
| Eccentricity: | 0.0025759 |
| inclination: | 86.3363° |
| perigee height: | 101 km |
| apogee height: | 134 km |
| right ascension of ascending node: | 249.3166° |
| argument of perigee: | 119.9357° |
| revolutions per day: | 16.58206397 |
| mean anomaly at epoch: | 245.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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