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 58411U 26145.53973286 +.00000000 +00000-0 +75517-4 0 00002
2 58411 43.0036 338.0873 0001524 265.7002 94.3676 15.27577240 08
| Epoch (UTC): | 25 May 2026 12:57:12 |
| Eccentricity: | 0.0001524 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.0873° |
| argument of perigee: | 265.7002° |
| revolutions per day: | 15.27577240 |
| mean anomaly at epoch: | 94.3676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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