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 58414U 26145.58343534 +.00000000 +00000-0 +17565-3 0 00005
2 58414 43.0033 338.4769 0001318 266.9978 93.0723 15.27582029 02
| Epoch (UTC): | 25 May 2026 14:00:08 |
| Eccentricity: | 0.0001318 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.4769° |
| argument of perigee: | 266.9978° |
| revolutions per day: | 15.27582029 |
| mean anomaly at epoch: | 93.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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