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 58906U 26145.35509880 +.00000000 +00000-0 +19897-3 0 00004
2 58906 49.9985 99.9754 0015109 272.7644 87.1564 14.83152726 05
| Epoch (UTC): | 25 May 2026 08:31:20 |
| Eccentricity: | 0.0015109 |
| inclination: | 49.9985° |
| perigee height: | 609 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 99.9754° |
| argument of perigee: | 272.7644° |
| revolutions per day: | 14.83152726 |
| mean anomaly at epoch: | 87.1564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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