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 58678U 26145.32291815 +.00000000 +00000-0 +36032-4 0 00004
2 58678 43.0052 12.5861 0000906 267.3169 92.7579 15.27576513 03
| Epoch (UTC): | 25 May 2026 07:45:00 |
| Eccentricity: | 0.0000906 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.5861° |
| argument of perigee: | 267.3169° |
| revolutions per day: | 15.27576513 |
| mean anomaly at epoch: | 92.7579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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