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 66350U 26145.54405801 +.00000000 +00000-0 +39503-3 0 00001
2 66350 53.1577 235.3876 0001189 292.5001 67.5873 15.30200847 08
| Epoch (UTC): | 25 May 2026 13:03:26 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.3876° |
| argument of perigee: | 292.5001° |
| revolutions per day: | 15.30200847 |
| mean anomaly at epoch: | 67.5873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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