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 66952U 26145.04751808 +.00000000 +00000-0 +93483-3 0 00002
2 66952 53.1605 3.3383 0000665 104.5622 255.5454 15.34412740 08
| Epoch (UTC): | 25 May 2026 01:08:25 |
| Eccentricity: | 0.0000665 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 3.3383° |
| argument of perigee: | 104.5622° |
| revolutions per day: | 15.34412740 |
| mean anomaly at epoch: | 255.5454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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