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 68475U 26145.32850539 +.00000000 +00000-0 +73219-3 0 00001
2 68475 97.7500 103.8476 0005466 113.0506 247.1289 14.91593664 07
| Epoch (UTC): | 25 May 2026 07:53:02 |
| Eccentricity: | 0.0005466 |
| inclination: | 97.7500° |
| perigee height: | 589 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.8476° |
| argument of perigee: | 113.0506° |
| revolutions per day: | 14.91593664 |
| mean anomaly at epoch: | 247.1289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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