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 66968U 26145.51142148 +.00000000 +00000-0 +66130-3 0 00001
2 66968 43.0006 309.8333 0000987 246.3664 113.7084 15.27600517 02
| Epoch (UTC): | 25 May 2026 12:16:26 |
| Eccentricity: | 0.0000987 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8333° |
| argument of perigee: | 246.3664° |
| revolutions per day: | 15.27600517 |
| mean anomaly at epoch: | 113.7084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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