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 58796U 26145.53608436 +.00000000 +00000-0 +29051-5 0 00003
2 58796 43.0009 91.6880 0000993 264.1449 95.9290 15.27575068 06
| Epoch (UTC): | 25 May 2026 12:51:57 |
| Eccentricity: | 0.0000993 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 91.6880° |
| argument of perigee: | 264.1449° |
| revolutions per day: | 15.27575068 |
| mean anomaly at epoch: | 95.9290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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