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 66505U 26145.65128980 +.00000000 +00000-0 +56180-3 0 00005
2 66505 43.0018 275.6726 0001270 274.6482 85.4225 15.27588960 05
| Epoch (UTC): | 25 May 2026 15:37:51 |
| Eccentricity: | 0.0001270 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 275.6726° |
| argument of perigee: | 274.6482° |
| revolutions per day: | 15.27588960 |
| mean anomaly at epoch: | 85.4225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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