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 67547U 26145.66053148 +.00000000 +00000-0 +88840-3 0 00004
2 67547 97.2865 32.7661 0002323 95.7815 264.3693 15.33453788 08
| Epoch (UTC): | 25 May 2026 15:51:09 |
| Eccentricity: | 0.0002323 |
| inclination: | 97.2865° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.7661° |
| argument of perigee: | 95.7815° |
| revolutions per day: | 15.33453788 |
| mean anomaly at epoch: | 264.3693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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