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 56292U 26145.02544545 +.00000000 +00000-0 +16431-4 0 00003
2 56292 43.0022 137.8820 0000975 280.6337 79.4405 15.27577334 09
| Epoch (UTC): | 25 May 2026 00:36:38 |
| Eccentricity: | 0.0000975 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 137.8820° |
| argument of perigee: | 280.6337° |
| revolutions per day: | 15.27577334 |
| mean anomaly at epoch: | 79.4405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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