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 66818U 26145.41414525 +.00000000 +00000-0 +70189-3 0 00004
2 66818 43.0011 41.0210 0000445 23.6995 336.3877 15.27588593 05
| Epoch (UTC): | 25 May 2026 09:56:22 |
| Eccentricity: | 0.0000445 |
| inclination: | 43.0011° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 41.0210° |
| argument of perigee: | 23.6995° |
| revolutions per day: | 15.27588593 |
| mean anomaly at epoch: | 336.3877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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