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 57782U 26145.41313255 +.00000000 +00000-0 +28626-5 0 00003
2 57782 43.0013 120.9390 0001104 264.6460 95.4266 15.27577947 06
| Epoch (UTC): | 25 May 2026 09:54:54 |
| Eccentricity: | 0.0001104 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.9390° |
| argument of perigee: | 264.6460° |
| revolutions per day: | 15.27577947 |
| mean anomaly at epoch: | 95.4266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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