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 47767U 26145.43074653 +.00000000 +00000-0 +11077-2 0 00002
2 47767 53.1560 200.6986 0006779 359.0875 1.0121 15.50150836 09
| Epoch (UTC): | 25 May 2026 10:20:16 |
| Eccentricity: | 0.0006779 |
| inclination: | 53.1560° |
| perigee height: | 412 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 200.6986° |
| argument of perigee: | 359.0875° |
| revolutions per day: | 15.50150836 |
| mean anomaly at epoch: | 1.0121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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