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 56546U 26145.47881103 +.00000000 +00000-0 +74024-3 0 00009
2 56546 43.0015 150.1242 0001315 257.5047 102.5657 15.27619120 06
| Epoch (UTC): | 25 May 2026 11:29:29 |
| Eccentricity: | 0.0001315 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1242° |
| argument of perigee: | 257.5047° |
| revolutions per day: | 15.27619120 |
| mean anomaly at epoch: | 102.5657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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