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 12U 59001B 24281.22075868 .00003911 00000-0 22987-2 0 9997
2 12 32.8971 241.0173 1652803 75.6326 302.1430 11.47227528702884
| Epoch (UTC): | 07 October 2024 05:17:53 |
| Eccentricity: | 0.1652803 |
| inclination: | 32.8971° |
| perigee height: | 553 km |
| apogee height: | 3298 km |
| right ascension of ascending node: | 241.0173° |
| argument of perigee: | 75.6326° |
| revolutions per day: | 11.47227528 |
| mean anomaly at epoch: | 302.1430° |
| orbit number at epoch: | 70288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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