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 56306U 26145.45357936 +.00000000 +00000-0 -72359-4 0 00004
2 56306 43.0009 135.0105 0001035 271.8082 88.2651 15.27585930 05
| Epoch (UTC): | 25 May 2026 10:53:09 |
| Eccentricity: | 0.0001035 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.0105° |
| argument of perigee: | 271.8082° |
| revolutions per day: | 15.27585930 |
| mean anomaly at epoch: | 88.2651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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