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 56839U 26145.09580288 +.00000000 +00000-0 +35988-4 0 00009
2 56839 43.0065 35.5285 0001301 255.6733 104.3975 15.27586471 00
| Epoch (UTC): | 25 May 2026 02:17:57 |
| Eccentricity: | 0.0001301 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 35.5285° |
| argument of perigee: | 255.6733° |
| revolutions per day: | 15.27586471 |
| mean anomaly at epoch: | 104.3975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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