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 66598U 26145.60852544 +.00000000 +00000-0 +78917-3 0 00004
2 66598 43.0036 341.4372 0001431 260.2503 99.8187 15.27582522 04
| Epoch (UTC): | 25 May 2026 14:36:16 |
| Eccentricity: | 0.0001431 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.4372° |
| argument of perigee: | 260.2503° |
| revolutions per day: | 15.27582522 |
| mean anomaly at epoch: | 99.8187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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