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 29252U 06029A 23156.60767511 .00008265 00000-0 31899-3 0 9991
2 29252 64.5206 347.2824 0026746 213.6751 146.2678 15.26597074932751
| Epoch (UTC): | 05 June 2023 14:35:03 |
| Eccentricity: | 0.0026746 |
| inclination: | 64.5206° |
| perigee height: | 467 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 347.2824° |
| argument of perigee: | 213.6751° |
| revolutions per day: | 15.26597074 |
| mean anomaly at epoch: | 146.2678° |
| orbit number at epoch: | 93275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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