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 58609U 26145.54582573 +.00000000 +00000-0 +74297-4 0 00001
2 58609 43.0025 94.9174 0001063 264.2907 95.7823 15.27574240 09
| Epoch (UTC): | 25 May 2026 13:05:59 |
| Eccentricity: | 0.0001063 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 94.9174° |
| argument of perigee: | 264.2907° |
| revolutions per day: | 15.27574240 |
| mean anomaly at epoch: | 95.7823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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