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 68529U 26145.26756656 +.00000000 +00000-0 +81794-3 0 00006
2 68529 53.1585 132.5630 0001378 69.7258 290.3893 15.34398641 03
| Epoch (UTC): | 25 May 2026 06:25:17 |
| Eccentricity: | 0.0001378 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.5630° |
| argument of perigee: | 69.7258° |
| revolutions per day: | 15.34398641 |
| mean anomaly at epoch: | 290.3893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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