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 49467U 21105D 24358.24418517 .00014577 00000-0 54240-3 0 9995
2 49467 74.9278 88.8549 0102462 264.1699 94.7817 15.22593681171246
| Epoch (UTC): | 23 December 2024 05:51:37 |
| Eccentricity: | 0.0102462 |
| inclination: | 74.9278° |
| perigee height: | 427 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 88.8549° |
| argument of perigee: | 264.1699° |
| revolutions per day: | 15.22593681 |
| mean anomaly at epoch: | 94.7817° |
| orbit number at epoch: | 17124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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