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 58853U 26145.44478382 +.00000000 +00000-0 +31297-4 0 00006
2 58853 43.0003 175.2282 0001153 281.2096 78.8626 15.27576972 04
| Epoch (UTC): | 25 May 2026 10:40:29 |
| Eccentricity: | 0.0001153 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.2282° |
| argument of perigee: | 281.2096° |
| revolutions per day: | 15.27576972 |
| mean anomaly at epoch: | 78.8626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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