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 67594U 26145.11620753 +.00000000 +00000-0 +65586-3 0 00000
2 67594 97.2836 210.1970 0000995 82.1176 278.0180 15.33454207 06
| Epoch (UTC): | 25 May 2026 02:47:20 |
| Eccentricity: | 0.0000995 |
| inclination: | 97.2836° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.1970° |
| argument of perigee: | 82.1176° |
| revolutions per day: | 15.33454207 |
| mean anomaly at epoch: | 278.0180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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