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 14453U 83109B 25198.90535668 .00000123 00000-0 43745-4 0 9998
2 14453 81.1657 14.9881 0104292 158.8732 201.6805 14.25357218168005
| Epoch (UTC): | 17 July 2025 21:43:42 |
| Eccentricity: | 0.0104292 |
| inclination: | 81.1657° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 14.9881° |
| argument of perigee: | 158.8732° |
| revolutions per day: | 14.25357218 |
| mean anomaly at epoch: | 201.6805° |
| orbit number at epoch: | 16800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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