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 56417U 26145.63454727 +.00000000 +00000-0 +26222-4 0 00000
2 56417 43.0057 112.3721 0001882 277.9638 82.1001 15.27578571 02
| Epoch (UTC): | 25 May 2026 15:13:44 |
| Eccentricity: | 0.0001882 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 112.3721° |
| argument of perigee: | 277.9638° |
| revolutions per day: | 15.27578571 |
| mean anomaly at epoch: | 82.1001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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