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 47760U 26145.60687978 +.00000000 +00000-0 +55171-5 0 00000
2 47760 53.1580 218.9616 0001129 78.4019 281.7109 15.31700347 02
| Epoch (UTC): | 25 May 2026 14:33:54 |
| Eccentricity: | 0.0001129 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 218.9616° |
| argument of perigee: | 78.4019° |
| revolutions per day: | 15.31700347 |
| mean anomaly at epoch: | 281.7109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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