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 27386U 02009A 21017.60598498 .00000017 00000-0 19068-4 0 9993
2 27386 98.1415 19.4295 0001194 85.7551 24.3095 14.38009017989329
| Epoch (UTC): | 17 January 2021 14:32:37 |
| Eccentricity: | 0.0001194 |
| inclination: | 98.1415° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 19.4295° |
| argument of perigee: | 85.7551° |
| revolutions per day: | 14.38009017 |
| mean anomaly at epoch: | 24.3095° |
| orbit number at epoch: | 98932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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