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 46556U 26145.33897632 +.00000000 +00000-0 +73337-3 0 00004
2 46556 53.0378 131.8915 0009478 29.1788 330.9754 15.66529879 04
| Epoch (UTC): | 25 May 2026 08:08:07 |
| Eccentricity: | 0.0009478 |
| inclination: | 53.0378° |
| perigee height: | 362 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 131.8915° |
| argument of perigee: | 29.1788° |
| revolutions per day: | 15.66529879 |
| mean anomaly at epoch: | 330.9754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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