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 65326U 26145.55455178 +.00000000 +00000-0 +53238-3 0 00007
2 65326 53.1585 209.8239 0001096 90.1079 270.0047 15.30197840 04
| Epoch (UTC): | 25 May 2026 13:18:33 |
| Eccentricity: | 0.0001096 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.8239° |
| argument of perigee: | 90.1079° |
| revolutions per day: | 15.30197840 |
| mean anomaly at epoch: | 270.0047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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