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 58358U 26145.40641304 +.00000000 +00000-0 +11767-3 0 00007
2 58358 43.0010 277.0632 0000979 265.4486 94.6254 15.27564950 00
| Epoch (UTC): | 25 May 2026 09:45:14 |
| Eccentricity: | 0.0000979 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.0632° |
| argument of perigee: | 265.4486° |
| revolutions per day: | 15.27564950 |
| mean anomaly at epoch: | 94.6254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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