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 56174U 26145.42310669 +.00000000 +00000-0 +00000-0 0 00005
2 56174 0.0144 296.8295 0001943 169.4664 198.0351 1.00268965 02
| Epoch (UTC): | 25 May 2026 10:09:16 |
| Eccentricity: | 0.0001943 |
| inclination: | 0.0144° |
| perigee height: | 35779 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 296.8295° |
| argument of perigee: | 169.4664° |
| revolutions per day: | 1.00268965 |
| mean anomaly at epoch: | 198.0351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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