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 14096U 83051B 24276.60565627 .00000477 00000-0 82788-3 0 9999
2 14096 72.3041 31.7462 1093474 45.8196 322.7593 12.09888184825907
| Epoch (UTC): | 02 October 2024 14:32:08 |
| Eccentricity: | 0.1093474 |
| inclination: | 72.3041° |
| perigee height: | 760 km |
| apogee height: | 2513 km |
| right ascension of ascending node: | 31.7462° |
| argument of perigee: | 45.8196° |
| revolutions per day: | 12.09888184 |
| mean anomaly at epoch: | 322.7593° |
| orbit number at epoch: | 82590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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