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 58679U 26145.04209649 +.00000000 +00000-0 +15181-3 0 00009
2 58679 43.0015 13.9157 0001547 276.9536 83.1140 15.27586443 03
| Epoch (UTC): | 25 May 2026 01:00:37 |
| Eccentricity: | 0.0001547 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 13.9157° |
| argument of perigee: | 276.9536° |
| revolutions per day: | 15.27586443 |
| mean anomaly at epoch: | 83.1140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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