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 33498U 09002G 25143.75101120 .00003850 00000-0 38820-3 0 9990
2 33498 98.1246 72.3947 0009777 24.1621 336.0053 14.91710591880764
| Epoch (UTC): | 23 May 2025 18:01:27 |
| Eccentricity: | 0.0009777 |
| inclination: | 98.1246° |
| perigee height: | 586 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 72.3947° |
| argument of perigee: | 24.1621° |
| revolutions per day: | 14.91710591 |
| mean anomaly at epoch: | 336.0053° |
| orbit number at epoch: | 88076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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