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 58717U 26145.42655910 +.00000000 +00000-0 +13850-4 0 00002
2 58717 53.1602 233.5435 0001034 98.8378 261.2740 15.30187070 07
| Epoch (UTC): | 25 May 2026 10:14:14 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.1602° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.5435° |
| argument of perigee: | 98.8378° |
| revolutions per day: | 15.30187070 |
| mean anomaly at epoch: | 261.2740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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