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 66191U 26145.26445204 +.00000000 +00000-0 +48281-3 0 00007
2 66191 53.1565 249.8589 0001248 86.7479 273.3665 15.30210840 07
| Epoch (UTC): | 25 May 2026 06:20:48 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.1565° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 249.8589° |
| argument of perigee: | 86.7479° |
| revolutions per day: | 15.30210840 |
| mean anomaly at epoch: | 273.3665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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