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 68531U 26145.24352929 +.00000000 +00000-0 +66952-3 0 00001
2 68531 53.1591 133.8274 0001327 69.1786 290.9357 15.30194185 09
| Epoch (UTC): | 25 May 2026 05:50:40 |
| Eccentricity: | 0.0001327 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.8274° |
| argument of perigee: | 69.1786° |
| revolutions per day: | 15.30194185 |
| mean anomaly at epoch: | 290.9357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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