Orbital Trajectory Models
Predict optimal orbital paths for satellites using over 20 different astrodynamics models
Predict optimal orbital paths for satellites using over 20 different astrodynamics models
Optimized for communication, observation, and scientific satellites in 200-2000km altitudes.
Models for 35,786km circular orbits synchronized with Earth's rotation.
Specialized Hohmann transfer and escape velocity calculations for missions beyond Earth's sphere of influence.
Our trajectory solver combines numerical integration, perturbation analysis, and optimization algorithms to calculate mission-critical paths.
High-precision numerical integration for orbital propagation
Includes J2, J3 gravitational harmonics and atmospheric drag
Applies differential corrections for optimal maneuvers
| Parameter | Description |
|---|---|
| Semi Major Axis | a = (rₐ + rₚ)/2 |
| Eccentricity | e = (rₐ - rₚ)/(rₐ + rₚ) |
| J2 Perturbation | Planetary gravitational harmonics correction |
| Delta-V Budget | Δv = sqrt(μ/(R_earth + h₁)) - sqrt(μ/(R_earth + h₂)) |
Calculate optimal launch windows for geosynchronous satellites with atmospheric and solar considerations.
Calculate Hohmann transfer parameters between differing circular orbits.
Model atmospheric re-entry paths for end-of-life satellites.
Our orbital models are accessible through REST API, WebSocket streaming, and downloadable SDKs for mission planning software integrations.
Access orbital data programmatically with our RESTful API using Python, JavaScript, or any HTTP-enabled environment.
curl -X POST https://api.orgbital7.com/orbit/prediction \
--header 'Content-Type: application/json' \
--data '{ "apogee": 6500, "perigee": 500, "missonType": "low-earth" }'
Download our C++, Python, and Rust SDKs for local orbit modeling and prediction capabilities in your mission control software.
Download SDKAccess peer-reviewed research on our orbital modeling algorithms and validation studies.
View PapersJoin our monthly webinar series with orbital dynamics experts to discuss complex trajectory scenarios.
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