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 58518U 26145.02706266 +.00000000 +00000-0 +90088-4 0 00006
2 58518 43.0021 32.5127 0001563 266.5534 93.5139 15.27587961 06
| Epoch (UTC): | 25 May 2026 00:38:58 |
| Eccentricity: | 0.0001563 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 32.5127° |
| argument of perigee: | 266.5534° |
| revolutions per day: | 15.27587961 |
| mean anomaly at epoch: | 93.5139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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