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 65647U 26145.16794481 +.00000000 +00000-0 +54762-3 0 00006
2 65647 53.1592 309.4700 0000792 90.4667 269.6429 15.42190855 06
| Epoch (UTC): | 25 May 2026 04:01:50 |
| Eccentricity: | 0.0000792 |
| inclination: | 53.1592° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 309.4700° |
| argument of perigee: | 90.4667° |
| revolutions per day: | 15.42190855 |
| mean anomaly at epoch: | 269.6429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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