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 61866U 26145.51288679 +.00000000 +00000-0 +17963-4 0 00004
2 61866 43.0039 164.4033 0001880 282.8079 77.2563 15.27577717 01
| Epoch (UTC): | 25 May 2026 12:18:33 |
| Eccentricity: | 0.0001880 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.4033° |
| argument of perigee: | 282.8079° |
| revolutions per day: | 15.27577717 |
| mean anomaly at epoch: | 77.2563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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