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 23265.47285543 .00000273 00000-0 10316-3 0 9999
2 27386 98.2423 231.5318 0001209 86.7492 24.4834 14.38409246129948
| Epoch (UTC): | 22 September 2023 11:20:54 |
| Eccentricity: | 0.0001209 |
| inclination: | 98.2423° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 231.5318° |
| argument of perigee: | 86.7492° |
| revolutions per day: | 14.38409246 |
| mean anomaly at epoch: | 24.4834° |
| orbit number at epoch: | 12994 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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