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 56924U 26145.63757353 +.00000000 +00000-0 +58527-5 0 00008
2 56924 43.0047 356.3437 0002141 293.1615 66.9011 15.27590355 07
| Epoch (UTC): | 25 May 2026 15:18:06 |
| Eccentricity: | 0.0002141 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.3437° |
| argument of perigee: | 293.1615° |
| revolutions per day: | 15.27590355 |
| mean anomaly at epoch: | 66.9011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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