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 58188U 26145.50795705 +.00000000 +00000-0 +38445-3 0 00006
2 58188 43.0058 69.5518 0001942 269.6002 90.4627 15.27550447 05
| Epoch (UTC): | 25 May 2026 12:11:27 |
| Eccentricity: | 0.0001942 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.5518° |
| argument of perigee: | 269.6002° |
| revolutions per day: | 15.27550447 |
| mean anomaly at epoch: | 90.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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