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 58635U 26145.55599973 +.00000000 +00000-0 +42891-4 0 00008
2 58635 43.0050 353.2932 0000712 292.1337 67.9439 15.27574686 04
| Epoch (UTC): | 25 May 2026 13:20:38 |
| Eccentricity: | 0.0000712 |
| inclination: | 43.0050° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 353.2932° |
| argument of perigee: | 292.1337° |
| revolutions per day: | 15.27574686 |
| mean anomaly at epoch: | 67.9439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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