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 56540U 26145.46162316 +.00000000 +00000-0 -21222-4 0 00004
2 56540 43.0021 153.4129 0001069 304.6821 55.3930 15.27584706 07
| Epoch (UTC): | 25 May 2026 11:04:44 |
| Eccentricity: | 0.0001069 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.4129° |
| argument of perigee: | 304.6821° |
| revolutions per day: | 15.27584706 |
| mean anomaly at epoch: | 55.3930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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