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 27387U 02009B 24287.91947513 .00000465 00000-0 17319-3 0 9999
2 27387 98.8091 280.6264 0033079 128.9087 231.5056 14.36506547185545
| Epoch (UTC): | 13 October 2024 22:04:02 |
| Eccentricity: | 0.0033079 |
| inclination: | 98.8091° |
| perigee height: | 746 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 280.6264° |
| argument of perigee: | 128.9087° |
| revolutions per day: | 14.36506547 |
| mean anomaly at epoch: | 231.5056° |
| orbit number at epoch: | 18554 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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