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 21021.79312870 .00000021 00000-0 20407-4 0 9990
2 27386 98.1419 23.3980 0001192 86.7625 86.8238 14.38009405989995
| Epoch (UTC): | 21 January 2021 19:02:06 |
| Eccentricity: | 0.0001192 |
| inclination: | 98.1419° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 23.3980° |
| argument of perigee: | 86.7625° |
| revolutions per day: | 14.38009405 |
| mean anomaly at epoch: | 86.8238° |
| orbit number at epoch: | 98999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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