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 66005U 26145.14703590 +.00000000 +00000-0 +64903-3 0 00002
2 66005 53.1607 108.6243 0001284 115.6497 244.4638 15.34407488 08
| Epoch (UTC): | 25 May 2026 03:31:43 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 108.6243° |
| argument of perigee: | 115.6497° |
| revolutions per day: | 15.34407488 |
| mean anomaly at epoch: | 244.4638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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