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 66382U 26145.59669053 +.00000000 +00000-0 +43040-3 0 00003
2 66382 53.1602 220.1325 0000853 51.0133 309.0943 15.30207820 04
| Epoch (UTC): | 25 May 2026 14:19:14 |
| Eccentricity: | 0.0000853 |
| inclination: | 53.1602° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.1325° |
| argument of perigee: | 51.0133° |
| revolutions per day: | 15.30207820 |
| mean anomaly at epoch: | 309.0943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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