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 26575U 00065A 18220.89676840 0.00000000 00000-0 00000-0 0 00
2 26575 6.8410 53.7526 0003644 18.1455 341.8925 1.00270000 07
| Epoch (UTC): | 08 August 2018 21:31:20 |
| Eccentricity: | 0.0003644 |
| inclination: | 6.8410° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 53.7526° |
| argument of perigee: | 18.1455° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 341.8925° |
| 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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