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 61544U 26145.46384471 +.00000000 +00000-0 +10188-4 0 00000
2 61544 53.1590 217.9312 0001169 79.3415 280.7734 15.69708206 01
| Epoch (UTC): | 25 May 2026 11:07:56 |
| Eccentricity: | 0.0001169 |
| inclination: | 53.1590° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 217.9312° |
| argument of perigee: | 79.3415° |
| revolutions per day: | 15.69708206 |
| mean anomaly at epoch: | 280.7734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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