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 56405U 26145.37814480 +.00000000 +00000-0 +25266-4 0 00001
2 56405 43.0047 113.8937 0001697 270.7848 89.2810 15.27577936 01
| Epoch (UTC): | 25 May 2026 09:04:31 |
| Eccentricity: | 0.0001697 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.8937° |
| argument of perigee: | 270.7848° |
| revolutions per day: | 15.27577936 |
| mean anomaly at epoch: | 89.2810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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