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 58273U 26145.21716684 +.00000000 +00000-0 +39549-3 0 00004
2 58273 97.3873 233.3874 0005226 226.4559 133.6258 15.48537971 00
| Epoch (UTC): | 25 May 2026 05:12:43 |
| Eccentricity: | 0.0005226 |
| inclination: | 97.3873° |
| perigee height: | 417 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 233.3874° |
| argument of perigee: | 226.4559° |
| revolutions per day: | 15.48537971 |
| mean anomaly at epoch: | 133.6258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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