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 56429U 26145.37009818 +.00000000 +00000-0 +24799-4 0 00008
2 56429 43.0036 106.7781 0001449 264.3713 95.6974 15.27574799 04
| Epoch (UTC): | 25 May 2026 08:52:56 |
| Eccentricity: | 0.0001449 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.7781° |
| argument of perigee: | 264.3713° |
| revolutions per day: | 15.27574799 |
| mean anomaly at epoch: | 95.6974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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