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 18267.71914694 +.00000028 +00000-0 +13421-3 0 9996
2 35498 082.4879 043.5912 0006531 219.2514 140.8091 12.40817736417657
| Epoch (UTC): | 24 September 2018 17:15:34 |
| Eccentricity: | 0.0006531 |
| inclination: | 82.4879° |
| perigee height: | 1498 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 43.5912° |
| argument of perigee: | 219.2514° |
| revolutions per day: | 12.40817736 |
| mean anomaly at epoch: | 140.8091° |
| orbit number at epoch: | 41765 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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