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 56538U 26145.63580233 +.00000000 +00000-0 +73643-5 0 00006
2 56538 43.0004 123.5464 0000961 268.8950 91.1791 15.27573961 03
| Epoch (UTC): | 25 May 2026 15:15:33 |
| Eccentricity: | 0.0000961 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 123.5464° |
| argument of perigee: | 268.8950° |
| revolutions per day: | 15.27573961 |
| mean anomaly at epoch: | 91.1791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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