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 66125U 26145.42494896 +.00000000 +00000-0 +40131-3 0 00009
2 66125 53.1607 42.8656 0001793 89.8119 270.3088 15.30204991 03
| Epoch (UTC): | 25 May 2026 10:11:55 |
| Eccentricity: | 0.0001793 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.8656° |
| argument of perigee: | 89.8119° |
| revolutions per day: | 15.30204991 |
| mean anomaly at epoch: | 270.3088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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