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 66597U 26145.24962139 +.00000000 +00000-0 +97315-3 0 00008
2 66597 43.0027 343.9055 0001116 282.2722 77.8005 15.27583291 04
| Epoch (UTC): | 25 May 2026 05:59:27 |
| Eccentricity: | 0.0001116 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.9055° |
| argument of perigee: | 282.2722° |
| revolutions per day: | 15.27583291 |
| mean anomaly at epoch: | 77.8005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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