CARD 01
Computational Proof
We certify the computation. You certify the inputs. Our math is provable. Your data stays your responsibility — and your property.
PROOF EMITTED
ENGINE NOMINAL
|
CUSTODY ZERO
|
CLASS ADVISORY
UTC --:--:--
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JD --
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FRAME GCRF/J2000
--
GEODESIC SPACE SYSTEMS
LLC · geodesicspacesystems.com
SEG ORBITAL COMPUTE
SURFACE HEADLESS API
UI NONE
ASTRODYNAMICS COMPUTE ENGINE
//
TIER-0
Compute at the
Speed of Flight.
Headless API SaaS Engine for Modern Astrodynamics & Spaceflight
Deterministic computational modules exposed as a pure machine interface — no console, no dashboards, no operator seat. Requests carry your state vectors in; certified mathematics and verification artifacts come back out. Nothing is retained on our side.
MODULES
09
GRAVITY HARMONICS
J2–J8
DATA CUSTODY
ZERO
FLIGHT CERT
NONE
ENGINE PARAMETERS
READ-ONLY
- CORE
- GDS-ENGINE
- INTERFACE
- REST / JSON
- TRANSPORT
- TLS 1.3
- EXECUTION
- DETERMINISTIC
- RETENTION
- NONE
- REFERENCE FRAME
- GCRF / J2000
- TIME SCALE
- TDB / UTC
- PUBLIC ENDPOINT
- --
- REGION BINDING
- UNKNOWN
- AVAILABILITY WINDOW
- --
UNPOPULATED FIELDS RENDER AS -- OR
UNKNOWN. NEVER AS ZERO.
SECTION A
Operational Charter
FOUR FOUNDATIONAL PRINCIPLES · BINDING ACROSS EVERY MODULE, EVERY REQUEST, EVERY RELEASE.
CARD 02
Zero Data Custody
Your data never leaves your side. Credentials, telemetry, mission files: stored here, never with us.
AT REST NONE
CARD 03
Invariant Physics
The physics cannot be switched off. Tier-0 variables sit beyond every password. Including ours.
TIER-0 LOCKED
CARD 04
Advisory Class
Advisory class. Mathematics is certified but not flight certified. We advise; you execute. Requires explicit FDO sign-off.
FDO SIGN-OFF REQUIRED
SECTION B
Core Computational Service Modules
09 FINALIZED ASTRODYNAMICS MODULES · EACH ADDRESSABLE AS AN INDEPENDENT HEADLESS ENDPOINT.
01
TRAJECTORY
Delta-V Fuel Optimization
Impulsive transfer trades, Lambert targeting, and optimal trajectory routing.
OUT ΔV [m/s] · LATENCY --
02
SAFETY
Conjunction & Debris Intelligence
Space object screening, collision probability (Pc), and automated avoidance advisories.
OUT Pc / MISS [km] · CATALOG UNKNOWN
03
DIAGNOSTIC
MicroKinetic Diagnostics
Telemetry force discrepancy analysis comparing physical telemetry against predicted orbital geodesics.
OUT RESIDUAL [m/s²] · BASELINE --
04
PROPAGATION
Harmonic Orbit Propagation
High-precision numerical propagation incorporating J2 through J8 spherical gravity harmonics.
OUT STATE VECTOR · STEP --
05
CONSTELLATION
Constellation Grid Harmonization
Slot placement, orbital resonance mapping, and station-keeping maintenance plans.
OUT SLOT PLAN · FLEET SIZE --
06
PROPULSION
Continuous Thrust
Low-thrust trajectory optimization for electric / chemical propulsion systems and long-duration orbit raising.
OUT THRUST ARC · Isp --
07
ENVIRONMENT
Space Weather Integration
Magnetospheric and atmospheric drag variation modeling using solar telemetry.
OUT DRAG PROFILE · F10.7 --
08
DEEP SPACE
Deep Space Relativistic Ephemeris
Decadal trajectory modeling out to Lagrange points, incorporating post-Newtonian relativistic corrections.
OUT EPHEMERIS · SPAN --
09
VERIFICATION
Deterministic Verification
Cryptographic computation proofs and Jacobi energy invariant logs for safety compliance audits.
OUT PROOF LOG · DIGEST --
SECTION C
Engine Characteristics
MODEL SURFACE AND OPERATIONAL BOUNDARIES · SUBJECT TO RELEASE-LEVEL VERIFICATION.
DYNAMICS MODEL
- GRAVITY FIELD
- J2–J8
- THIRD BODY
- SUN + MOON
- DRAG
- SOLAR-DRIVEN
- RELATIVITY
- POST-NEWTONIAN
- SRP COEFFICIENT
- --
- INTEGRATOR ORDER
- UNKNOWN
DATA POSTURE
- STORAGE AT REST
- NONE
- TELEMETRY COPIES
- 0 RETAINED
- CREDENTIAL VAULT
- CLIENT-SIDE
- MISSION FILES
- CLIENT-SIDE
- TRAINING USE
- PROHIBITED
- EXPORT CONTROL
- UNKNOWN
VERIFICATION SURFACE
- RUN REPRODUCIBILITY
- BIT-EXACT
- JACOBI INVARIANT
- LOGGED
- PROOF ARTIFACT
- CRYPTOGRAPHIC
- AUDIT TRAIL
- CLIENT-HELD
- FLIGHT CERTIFICATION
- NOT HELD
- ACCREDITATION ID
- --
ADVISORY CLASS NOTICE
Outputs are advisory computational products. Mathematics is certified; the system is not flight certified and carries no airworthiness, launch, or operational authority. All maneuver, avoidance, and station-keeping decisions require explicit Flight Dynamics Officer sign-off within the operator's own certified process. Simulated or unpopulated parameters are surfaced as -- or UNKNOWN and must never be interpreted as nominal values.