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 66558U 26145.04929336 +.00000000 +00000-0 +61512-3 0 00005
2 66558 43.0048 276.2014 0001029 302.4900 57.5853 15.27595023 05
| Epoch (UTC): | 25 May 2026 01:10:58 |
| Eccentricity: | 0.0001029 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.2014° |
| argument of perigee: | 302.4900° |
| revolutions per day: | 15.27595023 |
| mean anomaly at epoch: | 57.5853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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