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 56400U 26145.63711907 +.00000000 +00000-0 +35818-4 0 00009
2 56400 43.0049 112.4045 0001868 280.6398 79.4243 15.27579183 00
| Epoch (UTC): | 25 May 2026 15:17:27 |
| Eccentricity: | 0.0001868 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 112.4045° |
| argument of perigee: | 280.6398° |
| revolutions per day: | 15.27579183 |
| mean anomaly at epoch: | 79.4243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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