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 62587U 26145.38207764 +.00000000 +00000-0 +14547-2 0 00009
2 62587 43.0017 24.0966 0000352 21.4709 338.6173 15.70884868 01
| Epoch (UTC): | 25 May 2026 09:10:11 |
| Eccentricity: | 0.0000352 |
| inclination: | 43.0017° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 24.0966° |
| argument of perigee: | 21.4709° |
| revolutions per day: | 15.70884868 |
| mean anomaly at epoch: | 338.6173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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