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 56456U 26145.18786123 +.00000000 +00000-0 -38311-4 0 00004
2 56456 70.0016 311.6186 0001962 271.3873 88.7061 14.98318556 07
| Epoch (UTC): | 25 May 2026 04:30:31 |
| Eccentricity: | 0.0001962 |
| inclination: | 70.0016° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 311.6186° |
| argument of perigee: | 271.3873° |
| revolutions per day: | 14.98318556 |
| mean anomaly at epoch: | 88.7061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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