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 27422U 02021B 16274.15353911 .00000004 00000-0 17407-4 0 9997
2 27422 98.2297 282.8729 0011119 289.8060 70.1924 14.29249619749538
| Epoch (UTC): | 30 September 2016 03:41:05 |
| Eccentricity: | 0.0011119 |
| inclination: | 98.2297° |
| perigee height: | 786 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 282.8729° |
| argument of perigee: | 289.8060° |
| revolutions per day: | 14.29249619 |
| mean anomaly at epoch: | 70.1924° |
| orbit number at epoch: | 74953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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