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 57447U 26145.41400251 +.00000000 +00000-0 +62457-4 0 00003
2 57447 43.0008 186.7361 0001247 280.7656 79.3055 15.27580739 00
| Epoch (UTC): | 25 May 2026 09:56:09 |
| Eccentricity: | 0.0001247 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.7361° |
| argument of perigee: | 280.7656° |
| revolutions per day: | 15.27580739 |
| mean anomaly at epoch: | 79.3055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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