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 64619U 26145.55173330 +.00000000 +00000-0 +64173-3 0 00008
2 64619 53.1585 338.1548 0001182 84.5954 275.5181 15.30200238 07
| Epoch (UTC): | 25 May 2026 13:14:29 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.1548° |
| argument of perigee: | 84.5954° |
| revolutions per day: | 15.30200238 |
| mean anomaly at epoch: | 275.5181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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