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 56404U 26145.26664885 +.00000000 +00000-0 +53715-5 0 00001
2 56404 43.0020 114.7718 0001335 267.8356 92.2343 15.27573472 04
| Epoch (UTC): | 25 May 2026 06:23:58 |
| Eccentricity: | 0.0001335 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.7718° |
| argument of perigee: | 267.8356° |
| revolutions per day: | 15.27573472 |
| mean anomaly at epoch: | 92.2343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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