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 53430U 26145.33190910 +.00000000 +00000-0 +36642-4 0 00007
2 53430 53.2133 120.0958 0001090 71.1771 288.9339 15.08841858 03
| Epoch (UTC): | 25 May 2026 07:57:56 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 120.0958° |
| argument of perigee: | 71.1771° |
| revolutions per day: | 15.08841858 |
| mean anomaly at epoch: | 288.9339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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