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 33493U 09002B 24280.65285404 .00089059 00000-0 31045-2 0 9999
2 33493 98.1890 338.5180 0010274 218.7657 141.2845 15.29231552856028
| Epoch (UTC): | 06 October 2024 15:40:06 |
| Eccentricity: | 0.0010274 |
| inclination: | 98.1890° |
| perigee height: | 471 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 338.5180° |
| argument of perigee: | 218.7657° |
| revolutions per day: | 15.29231552 |
| mean anomaly at epoch: | 141.2845° |
| orbit number at epoch: | 85602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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