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 56409U 26145.33460572 +.00000000 +00000-0 +18704-4 0 00009
2 56409 43.0022 114.4228 0000874 259.5762 100.4991 15.27574295 05
| Epoch (UTC): | 25 May 2026 08:01:49 |
| Eccentricity: | 0.0000874 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.4228° |
| argument of perigee: | 259.5762° |
| revolutions per day: | 15.27574295 |
| mean anomaly at epoch: | 100.4991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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