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 56507U 26145.37263316 +.00000000 +00000-0 +71597-4 0 00008
2 56507 43.0029 106.6583 0001216 260.8084 99.2631 15.27585344 04
| Epoch (UTC): | 25 May 2026 08:56:35 |
| Eccentricity: | 0.0001216 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.6583° |
| argument of perigee: | 260.8084° |
| revolutions per day: | 15.27585344 |
| mean anomaly at epoch: | 99.2631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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