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 66190U 26145.57836275 +.00000000 +00000-0 +19199-3 0 00008
2 66190 53.1577 248.2665 0001224 87.6901 272.4240 15.30199176 08
| Epoch (UTC): | 25 May 2026 13:52:50 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2665° |
| argument of perigee: | 87.6901° |
| revolutions per day: | 15.30199176 |
| mean anomaly at epoch: | 272.4240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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