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 56545U 26145.47110324 +.00000000 +00000-0 -13333-3 0 00005
2 56545 43.0053 150.0718 0003253 266.7296 93.3184 15.27585245 07
| Epoch (UTC): | 25 May 2026 11:18:23 |
| Eccentricity: | 0.0003253 |
| inclination: | 43.0053° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 150.0718° |
| argument of perigee: | 266.7296° |
| revolutions per day: | 15.27585245 |
| mean anomaly at epoch: | 93.3184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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