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 12465U 81046B 22227.84830759 .00001965 00000-0 98559-4 0 9997
2 12465 81.2432 15.6219 0033657 132.5228 227.8853 15.16342121239815
| Epoch (UTC): | 15 August 2022 20:21:33 |
| Eccentricity: | 0.0033657 |
| inclination: | 81.2432° |
| perigee height: | 494 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 15.6219° |
| argument of perigee: | 132.5228° |
| revolutions per day: | 15.16342121 |
| mean anomaly at epoch: | 227.8853° |
| orbit number at epoch: | 23981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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