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 47568U 26145.58100878 +.00000000 +00000-0 +74278-3 0 00009
2 47568 53.0419 344.6032 0001563 188.7038 171.3955 15.77451233 05
| Epoch (UTC): | 25 May 2026 13:56:39 |
| Eccentricity: | 0.0001563 |
| inclination: | 53.0419° |
| perigee height: | 337 km |
| apogee height: | 339 km |
| right ascension of ascending node: | 344.6032° |
| argument of perigee: | 188.7038° |
| revolutions per day: | 15.77451233 |
| mean anomaly at epoch: | 171.3955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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