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 24357.62986008 .00003413 00000-0 17693-3 0 9998
2 33505 82.3862 29.8555 0024090 106.1237 254.2650 15.15596576875314
| Epoch (UTC): | 22 December 2024 15:06:59 |
| Eccentricity: | 0.0024090 |
| inclination: | 82.3862° |
| perigee height: | 502 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 29.8555° |
| argument of perigee: | 106.1237° |
| revolutions per day: | 15.15596576 |
| mean anomaly at epoch: | 254.2650° |
| orbit number at epoch: | 87531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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