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 27387U 02009B 23266.51447870 .00000206 00000-0 85833-4 0 9992
2 27387 98.7716 246.3151 0032055 189.0168 171.0446 14.36246057130079
| Epoch (UTC): | 23 September 2023 12:20:50 |
| Eccentricity: | 0.0032055 |
| inclination: | 98.7716° |
| perigee height: | 748 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 246.3151° |
| argument of perigee: | 189.0168° |
| revolutions per day: | 14.36246057 |
| mean anomaly at epoch: | 171.0446° |
| orbit number at epoch: | 13007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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