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 65409U 26145.52277250 +.00000000 +00000-0 +18941-3 0 00001
2 65409 53.1579 235.0510 0000945 83.8145 276.2964 15.31702453 06
| Epoch (UTC): | 25 May 2026 12:32:47 |
| Eccentricity: | 0.0000945 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.0510° |
| argument of perigee: | 83.8145° |
| revolutions per day: | 15.31702453 |
| mean anomaly at epoch: | 276.2964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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