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 41456U 26142.69623505 +.00000000 +00000-0 +12477-3 0 00008
2 41456 98.0909 202.4729 0016274 213.9941 146.0240 14.99073369 00
| Epoch (UTC): | 22 May 2026 16:42:34 |
| Eccentricity: | 0.0016274 |
| inclination: | 98.0909° |
| perigee height: | 558 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 202.4729° |
| argument of perigee: | 213.9941° |
| revolutions per day: | 14.99073369 |
| mean anomaly at epoch: | 146.0240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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