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 56309U 26145.49312352 +.00000000 +00000-0 +40677-3 0 00000
2 56309 9.9919 232.3101 0004377 138.0254 222.0298 15.21502101 01
| Epoch (UTC): | 25 May 2026 11:50:05 |
| Eccentricity: | 0.0004377 |
| inclination: | 9.9919° |
| perigee height: | 498 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 232.3101° |
| argument of perigee: | 138.0254° |
| revolutions per day: | 15.21502101 |
| mean anomaly at epoch: | 222.0298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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