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 68474U 26145.62144847 +.00000000 +00000-0 +21922-3 0 00005
2 68474 97.7538 104.2483 0001899 12.1024 348.0241 14.92460569 07
| Epoch (UTC): | 25 May 2026 14:54:53 |
| Eccentricity: | 0.0001899 |
| inclination: | 97.7538° |
| perigee height: | 589 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 104.2483° |
| argument of perigee: | 12.1024° |
| revolutions per day: | 14.92460569 |
| mean anomaly at epoch: | 348.0241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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