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 56397U 26145.40512964 +.00000000 +00000-0 +14817-4 0 00007
2 56397 43.0019 114.0969 0000856 267.2090 92.8663 15.27575791 07
| Epoch (UTC): | 25 May 2026 09:43:23 |
| Eccentricity: | 0.0000856 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.0969° |
| argument of perigee: | 267.2090° |
| revolutions per day: | 15.27575791 |
| mean anomaly at epoch: | 92.8663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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