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 56394U 26145.61784647 +.00000000 +00000-0 +41366-4 0 00005
2 56394 43.0028 112.2672 0001171 266.0577 94.0140 15.27575404 08
| Epoch (UTC): | 25 May 2026 14:49:41 |
| Eccentricity: | 0.0001171 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 112.2672° |
| argument of perigee: | 266.0577° |
| revolutions per day: | 15.27575404 |
| mean anomaly at epoch: | 94.0140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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