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 56425U 26145.35471436 +.00000000 +00000-0 +40027-4 0 00003
2 56425 43.0059 106.6720 0001431 294.1150 65.9552 15.26743919 07
| Epoch (UTC): | 25 May 2026 08:30:47 |
| Eccentricity: | 0.0001431 |
| inclination: | 43.0059° |
| perigee height: | 485 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 106.6720° |
| argument of perigee: | 294.1150° |
| revolutions per day: | 15.26743919 |
| mean anomaly at epoch: | 65.9552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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