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 23266.92458094 .00000269 00000-0 10180-3 0 9997
2 27386 98.2427 232.9260 0001168 86.5811 337.7189 14.38410146130159
| Epoch (UTC): | 23 September 2023 22:11:23 |
| Eccentricity: | 0.0001168 |
| inclination: | 98.2427° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 232.9260° |
| argument of perigee: | 86.5811° |
| revolutions per day: | 14.38410146 |
| mean anomaly at epoch: | 337.7189° |
| orbit number at epoch: | 13015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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