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 66932U 26145.31437745 +.00000000 +00000-0 +60475-3 0 00006
2 66932 53.1604 2.1645 0001462 86.2036 273.9134 15.34403741 04
| Epoch (UTC): | 25 May 2026 07:32:42 |
| Eccentricity: | 0.0001462 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 2.1645° |
| argument of perigee: | 86.2036° |
| revolutions per day: | 15.34403741 |
| mean anomaly at epoch: | 273.9134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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