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 58139U 26145.46950878 +.00000000 +00000-0 -46338-4 0 00003
2 58139 43.0033 58.5213 0000635 279.7916 80.2864 15.27585263 02
| Epoch (UTC): | 25 May 2026 11:16:05 |
| Eccentricity: | 0.0000635 |
| inclination: | 43.0033° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 58.5213° |
| argument of perigee: | 279.7916° |
| revolutions per day: | 15.27585263 |
| mean anomaly at epoch: | 80.2864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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