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 12185U 78026AA 23340.68398358 .00001165 00000-0 60878-3 0 9997
2 12185 99.1508 285.6296 0094988 21.5462 99.4436 14.14171787198641
| Epoch (UTC): | 06 December 2023 16:24:56 |
| Eccentricity: | 0.0094988 |
| inclination: | 99.1508° |
| perigee height: | 776 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 285.6296° |
| argument of perigee: | 21.5462° |
| revolutions per day: | 14.14171787 |
| mean anomaly at epoch: | 99.4436° |
| orbit number at epoch: | 19864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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