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 64178U 26145.55473911 +.00000000 +00000-0 +51666-3 0 00009
2 64178 53.1562 94.0905 0001381 94.9092 265.2066 15.30199142 05
| Epoch (UTC): | 25 May 2026 13:18:49 |
| Eccentricity: | 0.0001381 |
| inclination: | 53.1562° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 94.0905° |
| argument of perigee: | 94.9092° |
| revolutions per day: | 15.30199142 |
| mean anomaly at epoch: | 265.2066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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