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 59656U 26145.53738544 +.00000000 +00000-0 +51891-4 0 00009
2 59656 43.0013 328.0103 0000989 263.0734 97.0006 15.27579338 04
| Epoch (UTC): | 25 May 2026 12:53:50 |
| Eccentricity: | 0.0000989 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 328.0103° |
| argument of perigee: | 263.0734° |
| revolutions per day: | 15.27579338 |
| mean anomaly at epoch: | 97.0006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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