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 66567U 26145.39149971 +.00000000 +00000-0 +56662-3 0 00002
2 66567 42.9964 273.6021 0000484 353.6205 6.4640 15.27591393 02
| Epoch (UTC): | 25 May 2026 09:23:45 |
| Eccentricity: | 0.0000484 |
| inclination: | 42.9964° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 273.6021° |
| argument of perigee: | 353.6205° |
| revolutions per day: | 15.27591393 |
| mean anomaly at epoch: | 6.4640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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