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 56410U 26145.35116178 +.00000000 +00000-0 +20734-4 0 00009
2 56410 43.0022 113.6927 0001002 273.3143 86.7594 15.27576459 04
| Epoch (UTC): | 25 May 2026 08:25:40 |
| Eccentricity: | 0.0001002 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.6927° |
| argument of perigee: | 273.3143° |
| revolutions per day: | 15.27576459 |
| mean anomaly at epoch: | 86.7594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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