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 35500U 09036C 19017.46799725 .00000028 00000-0 13140-3 0 9990
2 35500 82.4905 329.9197 0006408 306.3090 53.7399 12.41458413432112
| Epoch (UTC): | 17 January 2019 11:13:54 |
| Eccentricity: | 0.0006408 |
| inclination: | 82.4905° |
| perigee height: | 1495 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 329.9197° |
| argument of perigee: | 306.3090° |
| revolutions per day: | 12.41458413 |
| mean anomaly at epoch: | 53.7399° |
| orbit number at epoch: | 43211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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