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 66458U 26145.51845208 +.00000000 +00000-0 +95203-3 0 00005
2 66458 42.9997 222.5230 0001734 284.8904 75.1756 15.27594556 07
| Epoch (UTC): | 25 May 2026 12:26:34 |
| Eccentricity: | 0.0001734 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.5230° |
| argument of perigee: | 284.8904° |
| revolutions per day: | 15.27594556 |
| mean anomaly at epoch: | 75.1756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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