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 58975U 26145.44049204 +.00000000 +00000-0 +29116-4 0 00005
2 58975 53.1608 300.2216 0001116 95.7630 264.3498 15.30194876 02
| Epoch (UTC): | 25 May 2026 10:34:18 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.2216° |
| argument of perigee: | 95.7630° |
| revolutions per day: | 15.30194876 |
| mean anomaly at epoch: | 264.3498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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