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 66390U 26145.49127227 +.00000000 +00000-0 +59736-3 0 00002
2 66390 53.1574 220.1656 0001236 75.2669 284.8468 15.30199958 00
| Epoch (UTC): | 25 May 2026 11:47:25 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.1656° |
| argument of perigee: | 75.2669° |
| revolutions per day: | 15.30199958 |
| mean anomaly at epoch: | 284.8468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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