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 58038U 26145.55038431 +.00000000 +00000-0 +34342-4 0 00004
2 58038 53.1608 78.5170 0001300 86.0130 274.1019 15.30197331 06
| Epoch (UTC): | 25 May 2026 13:12:33 |
| Eccentricity: | 0.0001300 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.5170° |
| argument of perigee: | 86.0130° |
| revolutions per day: | 15.30197331 |
| mean anomaly at epoch: | 274.1019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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