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 60126U 26145.41388907 +.00000000 +00000-0 +17184-4 0 00001
2 60126 53.1605 30.3124 0001243 83.5610 276.5532 15.30189801 09
| Epoch (UTC): | 25 May 2026 09:56:00 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.3124° |
| argument of perigee: | 83.5610° |
| revolutions per day: | 15.30189801 |
| mean anomaly at epoch: | 276.5532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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