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 56419U 26145.39100441 +.00000000 +00000-0 +14306-3 0 00005
2 56419 43.0018 113.9854 0000853 255.0187 105.0570 15.27573144 05
| Epoch (UTC): | 25 May 2026 09:23:02 |
| Eccentricity: | 0.0000853 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.9854° |
| argument of perigee: | 255.0187° |
| revolutions per day: | 15.27573144 |
| mean anomaly at epoch: | 105.0570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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