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 66731U 26145.45462400 +.00000000 +00000-0 +27090-3 0 00000
2 66731 97.4183 219.2494 0006179 94.4694 265.7246 15.19343703 05
| Epoch (UTC): | 25 May 2026 10:54:39 |
| Eccentricity: | 0.0006179 |
| inclination: | 97.4183° |
| perigee height: | 504 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 219.2494° |
| argument of perigee: | 94.4694° |
| revolutions per day: | 15.19343703 |
| mean anomaly at epoch: | 265.7246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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