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 66468U 26145.26460832 +.00000000 +00000-0 +57675-4 0 00006
2 66468 42.9991 224.0523 0000791 269.3403 90.7358 15.27576148 06
| Epoch (UTC): | 25 May 2026 06:21:02 |
| Eccentricity: | 0.0000791 |
| inclination: | 42.9991° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 224.0523° |
| argument of perigee: | 269.3403° |
| revolutions per day: | 15.27576148 |
| mean anomaly at epoch: | 90.7358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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