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 58850U 26145.59489302 +.00000000 +00000-0 +38464-3 0 00005
2 58850 58.6930 297.6000 0420983 82.1937 282.6658 14.43687327 01
| Epoch (UTC): | 25 May 2026 14:16:38 |
| Eccentricity: | 0.0420983 |
| inclination: | 58.6930° |
| perigee height: | 446 km |
| apogee height: | 1046 km |
| right ascension of ascending node: | 297.6000° |
| argument of perigee: | 82.1937° |
| revolutions per day: | 14.43687327 |
| mean anomaly at epoch: | 282.6658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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