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 56547U 26145.45697079 +.00000000 +00000-0 +13389-4 0 00003
2 56547 43.0030 149.9610 0001048 309.2231 50.8528 15.27577792 02
| Epoch (UTC): | 25 May 2026 10:58:02 |
| Eccentricity: | 0.0001048 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.9610° |
| argument of perigee: | 309.2231° |
| revolutions per day: | 15.27577792 |
| mean anomaly at epoch: | 50.8528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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