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 54508U 22151JL 24284.60394122 .04205041 00000-0 43738-1 0 9992
2 54508 98.6430 328.7104 0019016 298.1377 61.7954 15.60152402 28573
| Epoch (UTC): | 10 October 2024 14:29:40 |
| Eccentricity: | 0.0019016 |
| inclination: | 98.6430° |
| perigee height: | 374 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 328.7104° |
| argument of perigee: | 298.1377° |
| revolutions per day: | 15.60152402 |
| mean anomaly at epoch: | 61.7954° |
| orbit number at epoch: | 2857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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