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 23148.87552929 .00000229 00000-0 88888-4 0 9999
2 27386 98.2296 119.6727 0001282 89.3280 331.8219 14.38348854113189
| Epoch (UTC): | 28 May 2023 21:00:45 |
| Eccentricity: | 0.0001282 |
| inclination: | 98.2296° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 119.6727° |
| argument of perigee: | 89.3280° |
| revolutions per day: | 14.38348854 |
| mean anomaly at epoch: | 331.8219° |
| orbit number at epoch: | 11318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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