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 16909U 86061B 24259.20307715 -.00000078 00000-0 13571-3 0 9999
2 16909 50.0169 320.9343 0011031 333.5472 60.9987 12.44479990732410
| Epoch (UTC): | 15 September 2024 04:52:25 |
| Eccentricity: | 0.0011031 |
| inclination: | 50.0169° |
| perigee height: | 1479 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 320.9343° |
| argument of perigee: | 333.5472° |
| revolutions per day: | 12.44479990 |
| mean anomaly at epoch: | 60.9987° |
| orbit number at epoch: | 73241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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