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 53556U 26145.22518436 +.00000000 +00000-0 -33274-4 0 00000
2 53556 53.2127 80.5365 0001570 83.6435 276.4736 15.08845815 05
| Epoch (UTC): | 25 May 2026 05:24:15 |
| Eccentricity: | 0.0001570 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 80.5365° |
| argument of perigee: | 83.6435° |
| revolutions per day: | 15.08845815 |
| mean anomaly at epoch: | 276.4736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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