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 66229U 26145.51501524 +.00000000 +00000-0 +68989-3 0 00002
2 66229 53.1592 232.9306 0001215 85.0241 275.0899 15.30200141 03
| Epoch (UTC): | 25 May 2026 12:21:37 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.9306° |
| argument of perigee: | 85.0241° |
| revolutions per day: | 15.30200141 |
| mean anomaly at epoch: | 275.0899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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