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 58689U 26145.31649723 +.00000000 +00000-0 +25639-3 0 00000
2 58689 43.0030 12.5335 0001012 267.7449 92.3287 15.27599636 04
| Epoch (UTC): | 25 May 2026 07:35:45 |
| Eccentricity: | 0.0001012 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.5335° |
| argument of perigee: | 267.7449° |
| revolutions per day: | 15.27599636 |
| mean anomaly at epoch: | 92.3287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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