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 58468U 26145.55865037 +.00000000 +00000-0 +87377-3 0 00006
2 58468 97.3292 229.1344 0004944 231.8029 128.2792 15.76879742 03
| Epoch (UTC): | 25 May 2026 13:24:27 |
| Eccentricity: | 0.0004944 |
| inclination: | 97.3292° |
| perigee height: | 336 km |
| apogee height: | 343 km |
| right ascension of ascending node: | 229.1344° |
| argument of perigee: | 231.8029° |
| revolutions per day: | 15.76879742 |
| mean anomaly at epoch: | 128.2792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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