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 47884U 26144.86783948 +.00000000 +00000-0 +78323-4 0 00001
2 47884 53.1584 286.7154 0001181 83.5440 276.5696 15.31687251 07
| Epoch (UTC): | 24 May 2026 20:49:41 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 286.7154° |
| argument of perigee: | 83.5440° |
| revolutions per day: | 15.31687251 |
| mean anomaly at epoch: | 276.5696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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