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 67546U 26145.44029390 +.00000000 +00000-0 +48062-3 0 00003
2 67546 97.2869 32.4526 0002001 85.5033 274.6438 15.33453588 09
| Epoch (UTC): | 25 May 2026 10:34:01 |
| Eccentricity: | 0.0002001 |
| inclination: | 97.2869° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.4526° |
| argument of perigee: | 85.5033° |
| revolutions per day: | 15.33453588 |
| mean anomaly at epoch: | 274.6438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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