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 18172.12890389 .00000013 00000-0 26691-4 0 9992
2 35500 82.4880 100.5854 0008198 39.5601 320.6075 12.41456071406013
| Epoch (UTC): | 21 June 2018 03:05:37 |
| Eccentricity: | 0.0008198 |
| inclination: | 82.4880° |
| perigee height: | 1494 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 100.5854° |
| argument of perigee: | 39.5601° |
| revolutions per day: | 12.41456071 |
| mean anomaly at epoch: | 320.6075° |
| orbit number at epoch: | 40601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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