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 58480U 26145.60508873 +.00000000 +00000-0 +89834-4 0 00009
2 58480 43.0024 348.9039 0000993 271.3267 88.7471 15.27579134 04
| Epoch (UTC): | 25 May 2026 14:31:19 |
| Eccentricity: | 0.0000993 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 348.9039° |
| argument of perigee: | 271.3267° |
| revolutions per day: | 15.27579134 |
| mean anomaly at epoch: | 88.7471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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