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 24252.49518285 .00000817 00000-0 28014-3 0 9998
2 27386 98.2906 210.7232 0001201 87.7315 21.5187 14.38664101180551
| Epoch (UTC): | 08 September 2024 11:53:03 |
| Eccentricity: | 0.0001201 |
| inclination: | 98.2906° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 210.7232° |
| argument of perigee: | 87.7315° |
| revolutions per day: | 14.38664101 |
| mean anomaly at epoch: | 21.5187° |
| orbit number at epoch: | 18055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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