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 24281.13005877 .00000954 00000-0 32468-3 0 9999
2 27386 98.2967 238.4040 0001294 89.1997 281.3106 14.38702259184677
| Epoch (UTC): | 07 October 2024 03:07:17 |
| Eccentricity: | 0.0001294 |
| inclination: | 98.2967° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 238.4040° |
| argument of perigee: | 89.1997° |
| revolutions per day: | 14.38702259 |
| mean anomaly at epoch: | 281.3106° |
| orbit number at epoch: | 18467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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