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 58204U 26144.71344794 +.00000000 +00000-0 +00000-0 0 00008
2 58204 2.4864 80.7584 0003439 102.0770 48.7777 1.00272607 08
| Epoch (UTC): | 24 May 2026 17:07:21 |
| Eccentricity: | 0.0003439 |
| inclination: | 2.4864° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 80.7584° |
| argument of perigee: | 102.0770° |
| revolutions per day: | 1.00272607 |
| mean anomaly at epoch: | 48.7777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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