The existing view compares the initial and final orbital planes at the impulsive burn point.
28.50 deg between planes
7.800 km/s
3.840 km/s
0.492
Delta-v burden
3,840.0 m/s
49.2% of the local orbital speed.
Why low speed helps
Plane-change cost scales with burn speed, so performing the rotation near apoapsis can reduce delta-v.
Delta-v
3.8400 km/s
3,840.0 m/s
Plane angle
28.500 deg
Between the initial and final orbital planes
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.
The existing view compares the initial and final orbital planes at the impulsive burn point.
28.50 deg between planes
7.800 km/s
3.840 km/s
0.492
Delta-v burden
3,840.0 m/s
49.2% of the local orbital speed.
Why low speed helps
Plane-change cost scales with burn speed, so performing the rotation near apoapsis can reduce delta-v.
Delta-v
3.8400 km/s
3,840.0 m/s
Plane angle
28.500 deg
Between the initial and final orbital planes
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.