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 47240U 26145.12437685 +.00000000 +00000-0 +00000-0 0 00004
2 47240 0.0410 114.6172 0004099 11.2626 76.4604 1.00272274 08
| Epoch (UTC): | 25 May 2026 02:59:06 |
| Eccentricity: | 0.0004099 |
| inclination: | 0.0410° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 114.6172° |
| argument of perigee: | 11.2626° |
| revolutions per day: | 1.00272274 |
| mean anomaly at epoch: | 76.4604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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