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 27691U 03008A 23339.22789512 .00000068 00000-0 00000-0 0 9996
2 27691 9.1050 50.9583 0002422 217.3939 117.3197 1.00270401 23678
| Epoch (UTC): | 05 December 2023 05:28:10 |
| Eccentricity: | 0.0002422 |
| inclination: | 9.1050° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 50.9583° |
| argument of perigee: | 217.3939° |
| revolutions per day: | 1.00270401 |
| mean anomaly at epoch: | 117.3197° |
| orbit number at epoch: | 2367 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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