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 66791U 26144.99113302 +.00000000 +00000-0 +68020-3 0 00006
2 66791 43.0006 43.8745 0001396 248.6492 111.4211 15.27596266 09
| Epoch (UTC): | 24 May 2026 23:47:13 |
| Eccentricity: | 0.0001396 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 43.8745° |
| argument of perigee: | 248.6492° |
| revolutions per day: | 15.27596266 |
| mean anomaly at epoch: | 111.4211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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