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 66230U 26145.53189920 +.00000000 +00000-0 +29524-3 0 00000
2 66230 53.1580 233.0370 0001117 89.0352 271.0777 15.30195562 04
| Epoch (UTC): | 25 May 2026 12:45:56 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.0370° |
| argument of perigee: | 89.0352° |
| revolutions per day: | 15.30195562 |
| mean anomaly at epoch: | 271.0777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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