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 64184U 26145.24504825 +.00000000 +00000-0 +40412-3 0 00008
2 64184 53.1599 95.7119 0001452 93.8852 266.2315 15.30206919 07
| Epoch (UTC): | 25 May 2026 05:52:52 |
| Eccentricity: | 0.0001452 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.7119° |
| argument of perigee: | 93.8852° |
| revolutions per day: | 15.30206919 |
| mean anomaly at epoch: | 266.2315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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