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 61547U 26145.35225002 +.00000000 +00000-0 +30992-4 0 00000
2 61547 53.1614 17.9012 0001142 95.9469 264.1662 15.30193351 03
| Epoch (UTC): | 25 May 2026 08:27:14 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 17.9012° |
| argument of perigee: | 95.9469° |
| revolutions per day: | 15.30193351 |
| mean anomaly at epoch: | 264.1662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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