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 41260U 00055FL 24279.15068515 .00016977 00000-0 83768-2 0 9992
2 41260 98.8007 353.8794 0026076 127.2812 233.0745 14.17291439454277
| Epoch (UTC): | 05 October 2024 03:36:59 |
| Eccentricity: | 0.0026076 |
| inclination: | 98.8007° |
| perigee height: | 816 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 353.8794° |
| argument of perigee: | 127.2812° |
| revolutions per day: | 14.17291439 |
| mean anomaly at epoch: | 233.0745° |
| orbit number at epoch: | 45427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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