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 47722U 26145.43763880 +.00000000 +00000-0 -41232-4 0 00009
2 47722 53.1576 194.0526 0001119 77.8939 282.2187 15.31679819 03
| Epoch (UTC): | 25 May 2026 10:30:11 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.0526° |
| argument of perigee: | 77.8939° |
| revolutions per day: | 15.31679819 |
| mean anomaly at epoch: | 282.2187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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