The existing 3D view shows how J2 precession rotates the orbit plane's node line about Earth.
Inclination
98.00 deg
Altitude
700 km
Annual node motion
351.79 deg/yr
Orbit period
98.77 min
RAAN rate
0.96317 deg/day
1.9457e-7 rad/s · eastward
Orbital period
98.77 min
Mean two-body period
Semi-major axis
7,078.1 km
Earth radius plus altitude
Semi-latus rectum
7,078.13 km
Orbit geometry used by the J2 model
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 3D view shows how J2 precession rotates the orbit plane's node line about Earth.
Inclination
98.00 deg
Altitude
700 km
Annual node motion
351.79 deg/yr
Orbit period
98.77 min
RAAN rate
0.96317 deg/day
1.9457e-7 rad/s · eastward
Orbital period
98.77 min
Mean two-body period
Semi-major axis
7,078.1 km
Earth radius plus altitude
Semi-latus rectum
7,078.13 km
Orbit geometry used by the J2 model
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.