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 20491U 90013D 24287.53151668 .00000499 00000-0 99109-3 0 9990
2 20491 99.0252 314.9458 0468562 153.4575 209.1372 13.03690966649321
| Epoch (UTC): | 13 October 2024 12:45:23 |
| Eccentricity: | 0.0468562 |
| inclination: | 99.0252° |
| perigee height: | 890 km |
| apogee height: | 1605 km |
| right ascension of ascending node: | 314.9458° |
| argument of perigee: | 153.4575° |
| revolutions per day: | 13.03690966 |
| mean anomaly at epoch: | 209.1372° |
| orbit number at epoch: | 64932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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