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 66906U 26145.01567838 +.00000000 +00000-0 +40221-3 0 00008
2 66906 51.6288 46.3270 0005398 104.2596 255.8997 15.60666563 02
| Epoch (UTC): | 25 May 2026 00:22:34 |
| Eccentricity: | 0.0005398 |
| inclination: | 51.6288° |
| perigee height: | 382 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 46.3270° |
| argument of perigee: | 104.2596° |
| revolutions per day: | 15.60666563 |
| mean anomaly at epoch: | 255.8997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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