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 23338.91119914 .00000274 00000-0 10338-3 0 9992
2 27386 98.2559 302.1116 0001308 83.7797 297.3184 14.38460261140434
| Epoch (UTC): | 04 December 2023 21:52:07 |
| Eccentricity: | 0.0001308 |
| inclination: | 98.2559° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 302.1116° |
| argument of perigee: | 83.7797° |
| revolutions per day: | 14.38460261 |
| mean anomaly at epoch: | 297.3184° |
| orbit number at epoch: | 14043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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