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 66352U 26145.52506373 +.00000000 +00000-0 +22041-3 0 00006
2 66352 53.1582 235.2632 0001159 89.9970 270.1164 15.30198118 07
| Epoch (UTC): | 25 May 2026 12:36:05 |
| Eccentricity: | 0.0001159 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.2632° |
| argument of perigee: | 89.9970° |
| revolutions per day: | 15.30198118 |
| mean anomaly at epoch: | 270.1164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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