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 33505U 09003B 24255.78947979 .00005579 00000-0 29881-3 0 9993
2 33505 82.3871 131.8624 0024409 97.4405 262.9601 15.14558101859896
| Epoch (UTC): | 11 September 2024 18:56:51 |
| Eccentricity: | 0.0024409 |
| inclination: | 82.3871° |
| perigee height: | 505 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 131.8624° |
| argument of perigee: | 97.4405° |
| revolutions per day: | 15.14558101 |
| mean anomaly at epoch: | 262.9601° |
| orbit number at epoch: | 85989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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