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 66463U 26145.50688530 +.00000000 +00000-0 +86910-3 0 00008
2 66463 42.9989 222.4299 0001577 274.0724 85.9947 15.27583839 07
| Epoch (UTC): | 25 May 2026 12:09:54 |
| Eccentricity: | 0.0001577 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.4299° |
| argument of perigee: | 274.0724° |
| revolutions per day: | 15.27583839 |
| mean anomaly at epoch: | 85.9947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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