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 58619U 26145.60982028 +.00000000 +00000-0 +31880-4 0 00009
2 58619 43.0028 352.8341 0000990 269.5626 90.5112 15.27574416 08
| Epoch (UTC): | 25 May 2026 14:38:08 |
| Eccentricity: | 0.0000990 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.8341° |
| argument of perigee: | 269.5626° |
| revolutions per day: | 15.27574416 |
| mean anomaly at epoch: | 90.5112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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