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 18171.76799458 +.00000011 +00000-0 +80520-5 0 9992
2 35498 082.4877 103.1364 0008284 069.8782 290.3197 12.40816711405750
| Epoch (UTC): | 20 June 2018 18:25:54 |
| Eccentricity: | 0.0008284 |
| inclination: | 82.4877° |
| perigee height: | 1496 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 103.1364° |
| argument of perigee: | 69.8782° |
| revolutions per day: | 12.40816711 |
| mean anomaly at epoch: | 290.3197° |
| orbit number at epoch: | 40575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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