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 68523U 26145.22758801 +.00000000 +00000-0 +61583-3 0 00004
2 68523 53.1609 132.3043 0001144 78.6543 281.4588 15.34397139 00
| Epoch (UTC): | 25 May 2026 05:27:43 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 132.3043° |
| argument of perigee: | 78.6543° |
| revolutions per day: | 15.34397139 |
| mean anomaly at epoch: | 281.4588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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