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 64177U 26145.24821508 +.00000000 +00000-0 +47270-3 0 00009
2 64177 53.1610 95.7351 0001592 72.7756 287.3419 15.30207218 07
| Epoch (UTC): | 25 May 2026 05:57:25 |
| Eccentricity: | 0.0001592 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.7351° |
| argument of perigee: | 72.7756° |
| revolutions per day: | 15.30207218 |
| mean anomaly at epoch: | 287.3419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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