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 18267.70832535 +.00000033 +00000-0 +17126-3 0 9994
2 35500 082.4889 041.1995 0007095 181.0681 179.0378 12.41457653417879
| Epoch (UTC): | 24 September 2018 16:59:59 |
| Eccentricity: | 0.0007095 |
| inclination: | 82.4889° |
| perigee height: | 1495 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 41.1995° |
| argument of perigee: | 181.0681° |
| revolutions per day: | 12.41457653 |
| mean anomaly at epoch: | 179.0378° |
| orbit number at epoch: | 41787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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