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 47792U 26145.56596161 +.00000000 +00000-0 +55900-4 0 00002
2 47792 53.1582 241.5858 0001304 71.3271 288.7872 15.31704130 04
| Epoch (UTC): | 25 May 2026 13:34:59 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 241.5858° |
| argument of perigee: | 71.3271° |
| revolutions per day: | 15.31704130 |
| mean anomaly at epoch: | 288.7872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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