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 66075U 26145.58361128 +.00000000 +00000-0 +44457-3 0 00006
2 66075 53.1582 248.1479 0000013 94.3032 265.7970 15.30204567 09
| Epoch (UTC): | 25 May 2026 14:00:24 |
| Eccentricity: | 0.0000013 |
| inclination: | 53.1582° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 248.1479° |
| argument of perigee: | 94.3032° |
| revolutions per day: | 15.30204567 |
| mean anomaly at epoch: | 265.7970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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