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 58134U 26145.17855066 +.00000000 +00000-0 -44327-5 0 00006
2 58134 43.0018 60.6277 0001044 258.2000 101.8735 15.27586799 07
| Epoch (UTC): | 25 May 2026 04:17:06 |
| Eccentricity: | 0.0001044 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 60.6277° |
| argument of perigee: | 258.2000° |
| revolutions per day: | 15.27586799 |
| mean anomaly at epoch: | 101.8735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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