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 29U 60002B 23150.45119624 .00000608 00000-0 11889-3 0 9996
2 29 48.3792 264.0024 0023563 163.9591 196.2072 14.75326132377599
| Epoch (UTC): | 30 May 2023 10:49:43 |
| Eccentricity: | 0.0023563 |
| inclination: | 48.3792° |
| perigee height: | 627 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 264.0024° |
| argument of perigee: | 163.9591° |
| revolutions per day: | 14.75326132 |
| mean anomaly at epoch: | 196.2072° |
| orbit number at epoch: | 37759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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