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 25194.48286434 .00000093 00000-0 31838-4 0 9997
2 14453 81.1654 19.4436 0104032 171.6359 188.6586 14.25356231167292
| Epoch (UTC): | 13 July 2025 11:35:19 |
| Eccentricity: | 0.0104032 |
| inclination: | 81.1654° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 19.4436° |
| argument of perigee: | 171.6359° |
| revolutions per day: | 14.25356231 |
| mean anomaly at epoch: | 188.6586° |
| orbit number at epoch: | 16729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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