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 29048U 06011B 23088.76692334 .00000943 00000-0 38334-3 0 9992
2 29048 71.9640 106.8474 0041421 69.5764 290.9814 14.29254586888790
| Epoch (UTC): | 29 March 2023 18:24:22 |
| Eccentricity: | 0.0041421 |
| inclination: | 71.9640° |
| perigee height: | 764 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 106.8474° |
| argument of perigee: | 69.5764° |
| revolutions per day: | 14.29254586 |
| mean anomaly at epoch: | 290.9814° |
| orbit number at epoch: | 88879 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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