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 66443U 26145.56350307 +.00000000 +00000-0 +52768-3 0 00004
2 66443 42.9989 200.5860 0001738 266.4485 93.6168 15.27592751 08
| Epoch (UTC): | 25 May 2026 13:31:26 |
| Eccentricity: | 0.0001738 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.5860° |
| argument of perigee: | 266.4485° |
| revolutions per day: | 15.27592751 |
| mean anomaly at epoch: | 93.6168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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