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 57624U 26145.60158109 +.00000000 +00000-0 +00000-0 0 00005
2 57624 15.1140 194.5198 0001066 83.0016 271.8848 1.00274011 00
| Epoch (UTC): | 25 May 2026 14:26:16 |
| Eccentricity: | 0.0001066 |
| inclination: | 15.1140° |
| perigee height: | 35781 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 194.5198° |
| argument of perigee: | 83.0016° |
| revolutions per day: | 1.00274011 |
| mean anomaly at epoch: | 271.8848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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