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 66147U 26145.48350500 +.00000000 +00000-0 +54356-3 0 00006
2 66147 53.1595 66.2737 0001274 71.3447 288.7692 15.30203798 05
| Epoch (UTC): | 25 May 2026 11:36:14 |
| Eccentricity: | 0.0001274 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 66.2737° |
| argument of perigee: | 71.3447° |
| revolutions per day: | 15.30203798 |
| mean anomaly at epoch: | 288.7692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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