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 17268.91078289 +.00000031 +00000-0 +15519-3 0 9993
2 35498 082.4849 269.3086 0005890 302.7485 057.3032 12.40816174372535
| Epoch (UTC): | 25 September 2017 21:51:31 |
| Eccentricity: | 0.0005890 |
| inclination: | 82.4849° |
| perigee height: | 1498 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 269.3086° |
| argument of perigee: | 302.7485° |
| revolutions per day: | 12.40816174 |
| mean anomaly at epoch: | 57.3032° |
| orbit number at epoch: | 37253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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