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 47736U 26145.59226512 +.00000000 +00000-0 +10054-2 0 00002
2 47736 53.0726 202.3399 0005027 359.3921 0.7077 15.42353777 01
| Epoch (UTC): | 25 May 2026 14:12:51 |
| Eccentricity: | 0.0005027 |
| inclination: | 53.0726° |
| perigee height: | 436 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 202.3399° |
| argument of perigee: | 359.3921° |
| revolutions per day: | 15.42353777 |
| mean anomaly at epoch: | 0.7077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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