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 26635U 00080A 18217.91583850 0.00000000 00000-0 00000-0 0 01
2 26635 8.4126 33.9148 0004662 200.4203 159.5727 1.00270000 08
| Epoch (UTC): | 05 August 2018 21:58:48 |
| Eccentricity: | 0.0004662 |
| inclination: | 8.4126° |
| perigee height: | 35767 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 33.9148° |
| argument of perigee: | 200.4203° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 159.5727° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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