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 24287.87722897 .00000607 00000-0 21158-3 0 9993
2 27386 98.2984 244.9293 0001379 89.0604 287.1374 14.38713386185648
| Epoch (UTC): | 13 October 2024 21:03:12 |
| Eccentricity: | 0.0001379 |
| inclination: | 98.2984° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 244.9293° |
| argument of perigee: | 89.0604° |
| revolutions per day: | 14.38713386 |
| mean anomaly at epoch: | 287.1374° |
| orbit number at epoch: | 18564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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