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 47178U 26145.34701185 +.00000000 +00000-0 +72915-3 0 00004
2 47178 53.0469 265.9778 0002946 45.5783 314.5474 15.69693089 07
| Epoch (UTC): | 25 May 2026 08:19:41 |
| Eccentricity: | 0.0002946 |
| inclination: | 53.0469° |
| perigee height: | 358 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 265.9778° |
| argument of perigee: | 45.5783° |
| revolutions per day: | 15.69693089 |
| mean anomaly at epoch: | 314.5474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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