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 29006U 62047F 24248.78872842 .00003471 00000-0 43955-3 0 9996
2 29006 58.3125 328.6997 0011121 142.7600 217.4216 14.83883743605017
| Epoch (UTC): | 04 September 2024 18:55:46 |
| Eccentricity: | 0.0011121 |
| inclination: | 58.3125° |
| perigee height: | 609 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 328.6997° |
| argument of perigee: | 142.7600° |
| revolutions per day: | 14.83883743 |
| mean anomaly at epoch: | 217.4216° |
| orbit number at epoch: | 60501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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