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 20438U 90005C 24279.18265999 .00000678 00000-0 27264-3 0 9999
2 20438 98.8756 314.3356 0009916 11.5556 30.8183 14.31473523811742
| Epoch (UTC): | 05 October 2024 04:23:01 |
| Eccentricity: | 0.0009916 |
| inclination: | 98.8756° |
| perigee height: | 780 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 314.3356° |
| argument of perigee: | 11.5556° |
| revolutions per day: | 14.31473523 |
| mean anomaly at epoch: | 30.8183° |
| orbit number at epoch: | 81174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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