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 64166U 26145.40890657 +.00000000 +00000-0 +42310-3 0 00006
2 64166 97.4453 196.7956 0002051 133.1150 227.0249 15.05672734 08
| Epoch (UTC): | 25 May 2026 09:48:49 |
| Eccentricity: | 0.0002051 |
| inclination: | 97.4453° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.7956° |
| argument of perigee: | 133.1150° |
| revolutions per day: | 15.05672734 |
| mean anomaly at epoch: | 227.0249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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