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 65351U 26145.45009905 +.00000000 +00000-0 +12120-2 0 00001
2 65351 53.1578 171.2312 0001295 66.0098 294.1040 15.34389522 06
| Epoch (UTC): | 25 May 2026 10:48:08 |
| Eccentricity: | 0.0001295 |
| inclination: | 53.1578° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 171.2312° |
| argument of perigee: | 66.0098° |
| revolutions per day: | 15.34389522 |
| mean anomaly at epoch: | 294.1040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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