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 56530U 26145.38968442 +.00000000 +00000-0 +43212-4 0 00000
2 56530 43.0037 113.8248 0001120 265.9061 94.1663 15.27579260 01
| Epoch (UTC): | 25 May 2026 09:21:08 |
| Eccentricity: | 0.0001120 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.8248° |
| argument of perigee: | 265.9061° |
| revolutions per day: | 15.27579260 |
| mean anomaly at epoch: | 94.1663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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