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 24285.86337024 .00000950 00000-0 32339-3 0 9998
2 27386 98.2979 242.9815 0001416 89.4454 302.2982 14.38711897185356
| Epoch (UTC): | 11 October 2024 20:43:15 |
| Eccentricity: | 0.0001416 |
| inclination: | 98.2979° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 242.9815° |
| argument of perigee: | 89.4454° |
| revolutions per day: | 14.38711897 |
| mean anomaly at epoch: | 302.2982° |
| orbit number at epoch: | 18535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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