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 59586U 26145.54450338 +.00000000 +00000-0 +17286-2 0 00002
2 59586 42.9919 243.6951 0017960 8.1053 352.0092 15.43841508 09
| Epoch (UTC): | 25 May 2026 13:04:05 |
| Eccentricity: | 0.0017960 |
| inclination: | 42.9919° |
| perigee height: | 423 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 243.6951° |
| argument of perigee: | 8.1053° |
| revolutions per day: | 15.43841508 |
| mean anomaly at epoch: | 352.0092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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