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 56396U 26145.36786602 +.00000000 +00000-0 +40701-4 0 00004
2 56396 43.0031 113.8270 0001399 285.6205 74.4492 15.27578955 08
| Epoch (UTC): | 25 May 2026 08:49:43 |
| Eccentricity: | 0.0001399 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.8270° |
| argument of perigee: | 285.6205° |
| revolutions per day: | 15.27578955 |
| mean anomaly at epoch: | 74.4492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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