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 47772U 26145.35061714 +.00000000 +00000-0 +10949-4 0 00002
2 47772 53.1590 220.7531 0001034 81.6974 278.4145 15.31701810 03
| Epoch (UTC): | 25 May 2026 08:24:53 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 220.7531° |
| argument of perigee: | 81.6974° |
| revolutions per day: | 15.31701810 |
| mean anomaly at epoch: | 278.4145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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