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 66217U 26145.53506632 +.00000000 +00000-0 +52703-3 0 00003
2 66217 53.1558 233.0589 0000513 38.4476 321.6561 15.30202524 00
| Epoch (UTC): | 25 May 2026 12:50:29 |
| Eccentricity: | 0.0000513 |
| inclination: | 53.1558° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.0589° |
| argument of perigee: | 38.4476° |
| revolutions per day: | 15.30202524 |
| mean anomaly at epoch: | 321.6561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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