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 is defined by the following mean orbital elements,
1 67566U 26145.43177486 +.00000000 +00000-0 +11723-2 0 00007
2 67566 97.2844 205.7364 0000899 102.5357 257.5986 15.33511501 09
| Epoch (UTC): | 25 May 2026 10:21:45 |
| Eccentricity: | 0.0000899 |
| inclination: | 97.2844° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.7364° |
| argument of perigee: | 102.5357° |
| revolutions per day: | 15.33511501 |
| mean anomaly at epoch: | 257.5986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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