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 14085U 83048B 25169.51251312 .00000064 00000-0 50132-4 0 9999
2 14085 82.9439 79.6478 0032632 208.7430 151.1930 13.76566365112514
| Epoch (UTC): | 18 June 2025 12:18:01 |
| Eccentricity: | 0.0032632 |
| inclination: | 82.9439° |
| perigee height: | 952 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 79.6478° |
| argument of perigee: | 208.7430° |
| revolutions per day: | 13.76566365 |
| mean anomaly at epoch: | 151.1930° |
| orbit number at epoch: | 11251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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