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 66532U 26145.59762236 +.00000000 +00000-0 +53352-3 0 00004
2 66532 42.9997 203.7625 0001437 269.8133 90.2554 15.27618351 00
| Epoch (UTC): | 25 May 2026 14:20:34 |
| Eccentricity: | 0.0001437 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 203.7625° |
| argument of perigee: | 269.8133° |
| revolutions per day: | 15.27618351 |
| mean anomaly at epoch: | 90.2554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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