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 54176U 26145.35582406 +.00000000 +00000-0 +40226-3 0 00004
2 54176 53.2141 19.8053 0001504 97.9030 262.2133 15.08808144 03
| Epoch (UTC): | 25 May 2026 08:32:23 |
| Eccentricity: | 0.0001504 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 19.8053° |
| argument of perigee: | 97.9030° |
| revolutions per day: | 15.08808144 |
| mean anomaly at epoch: | 262.2133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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