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 29051U 06011E 23088.68402868 .00001130 00000-0 44772-3 0 9990
2 29051 72.0055 184.4928 0068961 327.5051 32.1848 14.29393267887169
| Epoch (UTC): | 29 March 2023 16:25:00 |
| Eccentricity: | 0.0068961 |
| inclination: | 72.0055° |
| perigee height: | 744 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 184.4928° |
| argument of perigee: | 327.5051° |
| revolutions per day: | 14.29393267 |
| mean anomaly at epoch: | 32.1848° |
| orbit number at epoch: | 88716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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