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 58919U 26144.82913705 +.00000000 +00000-0 +93072-3 0 00001
2 58919 97.3150 233.3971 0004954 225.4530 134.6331 15.75668073 09
| Epoch (UTC): | 24 May 2026 19:53:57 |
| Eccentricity: | 0.0004954 |
| inclination: | 97.3150° |
| perigee height: | 339 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 233.3971° |
| argument of perigee: | 225.4530° |
| revolutions per day: | 15.75668073 |
| mean anomaly at epoch: | 134.6331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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