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 65407U 26145.63044764 +.00000000 +00000-0 +55511-3 0 00007
2 65407 53.1565 235.0111 0001431 89.5213 270.5951 15.30201314 08
| Epoch (UTC): | 25 May 2026 15:07:50 |
| Eccentricity: | 0.0001431 |
| inclination: | 53.1565° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.0111° |
| argument of perigee: | 89.5213° |
| revolutions per day: | 15.30201314 |
| mean anomaly at epoch: | 270.5951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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