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 58625U 26145.00721095 +.00000000 +00000-0 +22312-3 0 00004
2 58625 43.0008 356.0510 0000882 266.4572 93.6179 15.27543452 06
| Epoch (UTC): | 25 May 2026 00:10:23 |
| Eccentricity: | 0.0000882 |
| inclination: | 43.0008° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.0510° |
| argument of perigee: | 266.4572° |
| revolutions per day: | 15.27543452 |
| mean anomaly at epoch: | 93.6179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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