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 56389U 26145.29861495 +.00000000 +00000-0 +21520-4 0 00000
2 56389 43.0016 125.4479 0001278 263.8202 96.2504 15.27578363 03
| Epoch (UTC): | 25 May 2026 07:10:00 |
| Eccentricity: | 0.0001278 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.4479° |
| argument of perigee: | 263.8202° |
| revolutions per day: | 15.27578363 |
| mean anomaly at epoch: | 96.2504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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