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 59958U 26145.21545462 +.00000000 +00000-0 +14661-3 0 00007
2 59958 53.1606 70.0221 0001303 94.8493 265.2657 15.30207825 01
| Epoch (UTC): | 25 May 2026 05:10:15 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 70.0221° |
| argument of perigee: | 94.8493° |
| revolutions per day: | 15.30207825 |
| mean anomaly at epoch: | 265.2657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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