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 24278.90574995 .00001096 00000-0 37088-3 0 9993
2 27386 98.2962 236.2531 0001308 89.3034 287.4858 14.38699021184351
| Epoch (UTC): | 04 October 2024 21:44:16 |
| Eccentricity: | 0.0001308 |
| inclination: | 98.2962° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 236.2531° |
| argument of perigee: | 89.3034° |
| revolutions per day: | 14.38699021 |
| mean anomaly at epoch: | 287.4858° |
| orbit number at epoch: | 18435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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