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 58709U 26145.56854334 +.00000000 +00000-0 -37535-5 0 00007
2 58709 53.1600 254.9153 0001007 101.5828 258.5303 15.69697216 06
| Epoch (UTC): | 25 May 2026 13:38:42 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 254.9153° |
| argument of perigee: | 101.5828° |
| revolutions per day: | 15.69697216 |
| mean anomaly at epoch: | 258.5303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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