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 61585U 26144.68022461 +.00000000 +00000-0 +11349-2 0 00004
2 61585 53.1574 281.7796 0001308 44.2335 315.8787 15.69726834 05
| Epoch (UTC): | 24 May 2026 16:19:31 |
| Eccentricity: | 0.0001308 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 281.7796° |
| argument of perigee: | 44.2335° |
| revolutions per day: | 15.69726834 |
| mean anomaly at epoch: | 315.8787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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