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 66141U 26145.41767105 +.00000000 +00000-0 +60361-3 0 00009
2 66141 53.1586 43.5264 0001128 86.2287 273.8843 15.30214138 00
| Epoch (UTC): | 25 May 2026 10:01:26 |
| Eccentricity: | 0.0001128 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.5264° |
| argument of perigee: | 86.2287° |
| revolutions per day: | 15.30214138 |
| mean anomaly at epoch: | 273.8843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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