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 59658U 26145.56679069 +.00000000 +00000-0 +27600-4 0 00001
2 59658 43.0030 327.3698 0001343 262.5363 97.5336 15.27584453 08
| Epoch (UTC): | 25 May 2026 13:36:10 |
| Eccentricity: | 0.0001343 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.3698° |
| argument of perigee: | 262.5363° |
| revolutions per day: | 15.27584453 |
| mean anomaly at epoch: | 97.5336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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