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 58732U 26145.45099124 +.00000000 +00000-0 +19089-4 0 00001
2 58732 43.0042 146.2276 0002009 279.6283 80.4342 15.27576722 01
| Epoch (UTC): | 25 May 2026 10:49:25 |
| Eccentricity: | 0.0002009 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.2276° |
| argument of perigee: | 279.6283° |
| revolutions per day: | 15.27576722 |
| mean anomaly at epoch: | 80.4342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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