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 60746U 26145.66349551 +.00000000 +00000-0 +41212-3 0 00006
2 60746 97.6748 284.2802 0009133 234.0152 126.0243 15.32670488 07
| Epoch (UTC): | 25 May 2026 15:55:26 |
| Eccentricity: | 0.0009133 |
| inclination: | 97.6748° |
| perigee height: | 462 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 284.2802° |
| argument of perigee: | 234.0152° |
| revolutions per day: | 15.32670488 |
| mean anomaly at epoch: | 126.0243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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