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 61956U 26145.26935139 +.00000000 +00000-0 +45189-3 0 00006
2 61956 53.1595 146.5468 0000514 98.5010 261.6049 15.30199593 07
| Epoch (UTC): | 25 May 2026 06:27:51 |
| Eccentricity: | 0.0000514 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.5468° |
| argument of perigee: | 98.5010° |
| revolutions per day: | 15.30199593 |
| mean anomaly at epoch: | 261.6049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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