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 47588U 26145.58511932 +.00000000 +00000-0 +98476-3 0 00004
2 47588 53.0308 312.3962 0009114 272.2993 87.6994 16.02301296 01
| Epoch (UTC): | 25 May 2026 14:02:34 |
| Eccentricity: | 0.0009114 |
| inclination: | 53.0308° |
| perigee height: | 262 km |
| apogee height: | 274 km |
| right ascension of ascending node: | 312.3962° |
| argument of perigee: | 272.2993° |
| revolutions per day: | 16.02301296 |
| mean anomaly at epoch: | 87.6994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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