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 58421U 26145.56544027 +.00000000 +00000-0 +73004-4 0 00002
2 58421 43.0074 338.3462 0002062 266.8652 93.1964 15.27576183 01
| Epoch (UTC): | 25 May 2026 13:34:14 |
| Eccentricity: | 0.0002062 |
| inclination: | 43.0074° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.3462° |
| argument of perigee: | 266.8652° |
| revolutions per day: | 15.27576183 |
| mean anomaly at epoch: | 93.1964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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