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 23337.87410774 .00000332 00000-0 12251-3 0 9995
2 27386 98.2558 301.1142 0001309 83.6227 330.0615 14.38459774140351
| Epoch (UTC): | 03 December 2023 20:58:42 |
| Eccentricity: | 0.0001309 |
| inclination: | 98.2558° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 301.1142° |
| argument of perigee: | 83.6227° |
| revolutions per day: | 14.38459774 |
| mean anomaly at epoch: | 330.0615° |
| orbit number at epoch: | 14035 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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