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 58593U 26145.26757853 +.00000000 +00000-0 +20708-4 0 00005
2 58593 43.0030 96.2828 0001266 288.7911 71.2804 15.27577993 05
| Epoch (UTC): | 25 May 2026 06:25:18 |
| Eccentricity: | 0.0001266 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.2828° |
| argument of perigee: | 288.7911° |
| revolutions per day: | 15.27577993 |
| mean anomaly at epoch: | 71.2804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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