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 51792U 26145.34064792 +.00000000 +00000-0 +38845-4 0 00002
2 51792 53.2143 5.0201 0001297 89.8564 270.2577 15.08837957 04
| Epoch (UTC): | 25 May 2026 08:10:31 |
| Eccentricity: | 0.0001297 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 5.0201° |
| argument of perigee: | 89.8564° |
| revolutions per day: | 15.08837957 |
| mean anomaly at epoch: | 270.2577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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