Asteroid Orbital Element File Generator

Generated Orbital Element Data (JSON)

// Orbital elements will be generated here.

Calculated Period (Years) 0.0

Pericenter Distance (AU) 0.0

The Six Classical Orbital Elements

Inputs are degrees (°) for angles and Astronomical Units (AU) for distances.

1. Semi-Major Axis (a) [AU]

2. Eccentricity (e) [0-1]

3. Inclination (i) [Degrees]

4. Longitude of Ascending Node (Ω) [Degrees]

5. Argument of Periapsis (ω) [Degrees]

6. Mean Anomaly (M) [Degrees]

Object Details

Object Name / Designation

Epoch Date (YYYY-MM-DD)

Output Settings

Output Format (For Copy/Export)

Assumed Central Body

Object: ${document.getElementById('aoefg-in-name').value} | Epoch: ${document.getElementById('aoefg-in-epoch').value}

Generated Data File (Format: ${document.getElementById('aoefg-cfg-format').value})

${originalCode}

Summary of Inputs

Semi-Major Axis (a): ${document.getElementById('aoefg-in-a').value} AU
Eccentricity (e): ${document.getElementById('aoefg-in-e').value}
Orbital Period (Calculated): ${document.getElementById('aoefg-out-period').innerText}

`; const opt = { margin: 0.5, filename: 'Orbital_Elements_Spec.pdf', image: { type: 'jpeg', quality: 0.98 }, html2canvas: { scale: 2 } }; html2pdf().set(opt).from(tempDiv).save(); }; })();