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 66127U 26145.41556084 +.00000000 +00000-0 +62545-3 0 00001
2 66127 53.1578 43.5156 0000737 85.8437 274.2648 15.30213012 00
| Epoch (UTC): | 25 May 2026 09:58:24 |
| Eccentricity: | 0.0000737 |
| inclination: | 53.1578° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.5156° |
| argument of perigee: | 85.8437° |
| revolutions per day: | 15.30213012 |
| mean anomaly at epoch: | 274.2648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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