ORBIT · E2E · v0.3 N 0°00′ · E 0°00′ · EARTH
POINT-TO-POINT · SUB-ORBITAL

EARTH TO EARTH

A Starship-class trajectory analyzer.
MAE 2.0 minutes, validated against six published routes.

EXPLORE →
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Chapter I · Scale

0 KM

The world is this big around. Commercial flies it in 48 hours. Starship compresses that ≈30×.

Commercial
0HRS
Starship E2E
~0MIN
Compression
0×
Chapter II · Physics

A ballistic arc
cuts straighter
than any great circle.

γ 13.5° · crosses Kármán · 30 min free-fall · near-orbital re-entry.

T-0 MECO Apex EI Touch
Chapter III · The Premise
"

I'm definitely excited about
San Francisco to Singapore in 55 minutes
or whatever the number ends up being.

Vitalik Buterin·NFX B-Sides·2021
Chapter IV · The Numbers

Validated against six routes.
Mean absolute error 2 min.

Semi-empirical ballistic model fitted to SpaceX published E2E timings. Maximum error across six routes is 2.8 min.

SFO SIN
0MIN
17h 40m commercialsaves 16h 45m
NYC SHA
0MIN
15h 15m commercialsaves 14h 36m
LAX NYC
0MIN
5h 45m commercialsaves 5h 20m
Mean Absolute Error
0.0MIN
Across 6 SpaceX-published routes from 7 100 km to 15 400 km. Fit computed live in browser.
Now pick any two cities

Build your own trajectory.

ORBIT / E2E
v0.3 TRAJECTORY ANALYZER
Input Parameters STARSHIP · E2E
Preset Routes
SFO → SIN
13,580km
ECEF · J2000
TRAJECTORY ▲
DRAG TO ROTATE · PINCH TO ZOOM
Estimated transit · Starship E2E
44:15min
vs. commercial air 17h 30m · saves 16h 46m (96%)
01
BOOST
4:50
Δv 8.6 km/s
02
COAST
30:18
0-g · 1818 s
03
ENTRY
6:00
EDL + land
Orbital Parameters semi-empirical · vs min-energy
d range 13,582km
θ angular 122.1°
v_cr cruise 7.80km/s
v_min min-energy 7.37km/s
Mach 22.7M
Q · v²R/μ 0.974
Apex altitude 85km
γ burnout 13.5°
Δv total 8.88km/s
Prop. fraction 0.89
Mass ratio 9.3
Isp avg 360s
Peak G · boost 3.5g
Peak G · entry 3.0g
Inclination i 47.6°
Azimuth 301°
Rot. Δv aid +0.31km/s
BC β 130kg/m²
Free-fall duration 29:48aboard
Flight Notes
AI Mission Analysis
ORBIT AI · v0.3
Running engineering review…
Risk Register ENGINEERING
Methodology
Great-circle distance: haversine (R = 6371.009 km, WGS-84 mean). Azimuth: forward bearing along geodesic. Inclination: from spherical trigonometry,cos i = cos(lat) · sin(az). Rotational Δv contribution:v_earth · sin(az) at launch latitude.

Ballistic trajectory solver: semi-empirical model combining Rauschenbakh minimum-energy formula Q = 2sin(θ/2) / (1 + sin(θ/2)) with SpaceX E2E flight-flattening correction factor f(d) fitted from published timings. Propellant mass fraction computed from Tsiolkovsky with Isp = 360s avg (Raptor vac/SL blend).

Source: SpaceX Starship · E2E specs. AI inference: ORBIT engineering model (server-side proxy).
Validation
Model vs SpaceX Published E2E Times
RouteSpaceXModelΔ
LA → NYC25.022.6−2.4
NYC → PAR30.027.2−2.8
SYD → SIN31.028.3−2.7
LA → LON32.033.6+1.6
LON → HK34.035.3+1.3
NYC → SHA39.040.3+1.3
MAE2.0 min
COPIED