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 58484U 26145.60380201 +.00000000 +00000-0 +49569-4 0 00007
2 58484 43.0053 348.8917 0001455 257.4602 102.6087 15.27573538 07
| Epoch (UTC): | 25 May 2026 14:29:28 |
| Eccentricity: | 0.0001455 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 348.8917° |
| argument of perigee: | 257.4602° |
| revolutions per day: | 15.27573538 |
| mean anomaly at epoch: | 102.6087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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