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 56539U 26145.45778353 +.00000000 +00000-0 +31796-3 0 00000
2 56539 43.0013 153.3824 0001852 309.8292 50.2397 15.27550839 07
| Epoch (UTC): | 25 May 2026 10:59:12 |
| Eccentricity: | 0.0001852 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.3824° |
| argument of perigee: | 309.8292° |
| revolutions per day: | 15.27550839 |
| mean anomaly at epoch: | 50.2397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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