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 data is extracted from the following two-line orbital elements,
1 39058U 13001B 23273.68595465 .00000024 00000-0 97607-4 0 9994
2 39058 82.4948 112.2357 0017077 20.0324 340.1423 12.43984318486138
| Epoch (UTC): | 30 September 2023 16:27:46 |
| Eccentricity: | 0.0017077 |
| inclination: | 82.4948° |
| perigee height: | 1476 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 112.2357° |
| argument of perigee: | 20.0324° |
| revolutions per day: | 12.43984318 |
| mean anomaly at epoch: | 340.1423° |
| orbit number at epoch: | 48613 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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