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 68476U 26145.35258098 +.00000000 +00000-0 +37681-3 0 00000
2 68476 97.7544 103.9937 0002427 26.2744 333.8598 14.92542445 00
| Epoch (UTC): | 25 May 2026 08:27:42 |
| Eccentricity: | 0.0002427 |
| inclination: | 97.7544° |
| perigee height: | 588 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 103.9937° |
| argument of perigee: | 26.2744° |
| revolutions per day: | 14.92542445 |
| mean anomaly at epoch: | 333.8598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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