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 data is extracted from the following two-line orbital elements,
1 35498U 09036A 17204.88951614 +.00000031 +00000-0 +15519-3 0 9991
2 35498 082.4911 309.0341 0007895 077.4405 282.7556 12.40815416364596
| Epoch (UTC): | 23 July 2017 21:20:54 |
| Eccentricity: | 0.0007895 |
| inclination: | 82.4911° |
| perigee height: | 1497 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 309.0341° |
| argument of perigee: | 77.4405° |
| revolutions per day: | 12.40815416 |
| mean anomaly at epoch: | 282.7556° |
| orbit number at epoch: | 36459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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