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 56391U 26145.39340045 +.00000000 +00000-0 +43730-4 0 00004
2 56391 43.0055 124.4391 0001579 283.6664 76.4011 15.27580868 03
| Epoch (UTC): | 25 May 2026 09:26:29 |
| Eccentricity: | 0.0001579 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.4391° |
| argument of perigee: | 283.6664° |
| revolutions per day: | 15.27580868 |
| mean anomaly at epoch: | 76.4011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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