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 11267U 79011B 24279.96153987 .00003913 00000-0 39491-3 0 9992
2 11267 82.5249 229.2619 0016229 359.4190 0.7007 14.90766344472518
| Epoch (UTC): | 05 October 2024 23:04:37 |
| Eccentricity: | 0.0016229 |
| inclination: | 82.5249° |
| perigee height: | 584 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 229.2619° |
| argument of perigee: | 359.4190° |
| revolutions per day: | 14.90766344 |
| mean anomaly at epoch: | 0.7007° |
| orbit number at epoch: | 47251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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