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 26474U 00047B 22224.83511099 .00001062 00000-0 10034-3 0 9992
2 26474 67.9929 70.0559 0051231 49.5384 311.0209 14.96984988196882
| Epoch (UTC): | 12 August 2022 20:02:33 |
| Eccentricity: | 0.0051231 |
| inclination: | 67.9929° |
| perigee height: | 540 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 70.0559° |
| argument of perigee: | 49.5384° |
| revolutions per day: | 14.96984988 |
| mean anomaly at epoch: | 311.0209° |
| orbit number at epoch: | 19688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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