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 23266.85337250 .00000260 00000-0 98814-4 0 9991
2 27386 98.2426 232.8576 0001191 86.7447 329.0321 14.38410029130141
| Epoch (UTC): | 23 September 2023 20:28:51 |
| Eccentricity: | 0.0001191 |
| inclination: | 98.2426° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 232.8576° |
| argument of perigee: | 86.7447° |
| revolutions per day: | 14.38410029 |
| mean anomaly at epoch: | 329.0321° |
| orbit number at epoch: | 13014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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