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 21016.56184573 .00000016 00000-0 18726-4 0 9991
2 27386 98.1414 18.4399 0001203 86.3018 21.5766 14.38008903989178
| Epoch (UTC): | 16 January 2021 13:29:03 |
| Eccentricity: | 0.0001203 |
| inclination: | 98.1414° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 18.4399° |
| argument of perigee: | 86.3018° |
| revolutions per day: | 14.38008903 |
| mean anomaly at epoch: | 21.5766° |
| orbit number at epoch: | 98917 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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