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 64778U 26145.59200154 +.00000000 +00000-0 -17948-4 0 00003
2 64778 53.1584 222.6670 0000897 87.5772 272.5331 15.30185281 02
| Epoch (UTC): | 25 May 2026 14:12:28 |
| Eccentricity: | 0.0000897 |
| inclination: | 53.1584° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.6670° |
| argument of perigee: | 87.5772° |
| revolutions per day: | 15.30185281 |
| mean anomaly at epoch: | 272.5331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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