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 59104U 26145.32997887 +.00000000 +00000-0 +17184-3 0 00007
2 59104 97.8373 275.9478 0007524 113.5685 246.6328 14.97091267 04
| Epoch (UTC): | 25 May 2026 07:55:10 |
| Eccentricity: | 0.0007524 |
| inclination: | 97.8373° |
| perigee height: | 571 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 275.9478° |
| argument of perigee: | 113.5685° |
| revolutions per day: | 14.97091267 |
| mean anomaly at epoch: | 246.6328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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