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 66184U 26145.57519639 +.00000000 +00000-0 +14455-3 0 00003
2 66184 53.1573 248.2463 0001744 299.4081 60.6746 15.30191803 09
| Epoch (UTC): | 25 May 2026 13:48:16 |
| Eccentricity: | 0.0001744 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2463° |
| argument of perigee: | 299.4081° |
| revolutions per day: | 15.30191803 |
| mean anomaly at epoch: | 60.6746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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