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 58179U 26145.51052211 +.00000000 +00000-0 +39514-4 0 00004
2 58179 43.0044 69.5759 0001201 269.6657 90.4057 15.27575773 07
| Epoch (UTC): | 25 May 2026 12:15:09 |
| Eccentricity: | 0.0001201 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.5759° |
| argument of perigee: | 269.6657° |
| revolutions per day: | 15.27575773 |
| mean anomaly at epoch: | 90.4057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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