ORBITS
/ GEOCENTRIC VISUALIZER
SGP4
NOMINAL
FRAME
ECI J2000
Target
/ 01
Preset catalog
Custom TLE
Random
TLE Input
/ 02
Two-Line Element (name optional)
Propagate
Cancel
Orbital Elements
/ 03
Class
—
Period
—
Perigee
—
Apogee
—
Incl.
—
Ecc.
—
Live Telemetry
/ 04
Altitude
—
km
Velocity
—
km/s
Latitude
—
Longitude
—
Ground Track
—
Equator
Polar
Follow
Orbit track
Current position
Ground trace
—
UTC
T+00:00:00
NOW
1×
1m/s
10m/s
1h/s
6h/s