LOADING

LOADING

LOADING

Paste 3-line TLE below:
See CelesTrak for available TLEs.

Paste a list of 3-line TLEs below:
See CelesTrak for available TLEs.

Select TLE from the list of satellites below:

Target Name
Insert TLE
Insert TLE List
Select TLE
Insert OSV
Export OSV
Data Source
Enable Clock
- Display
- Grid Lines
- Map Lines
- Textures
- Show Visibility
- Subsolar Point
- Orbit Lines
- Sun Orbit
- Show List
- Grid Lon. Resolution
- Grid Lat. Resolution
- Orbits Before
- Orbits After
- Points per Orbit
- Satellite Scaling
- Point Size
- Grid Color
- Map Color
- Orbit Color
- Point Color
- Camera
- Frame
- Field of View
- Lock Longitude
- Lock Latitude
- Longitude
- Latitude
- Distance
- Longitude Up
- Latitude Up
- Time
- Warp Size
- Time Warp
- Year
- Month
- Day
- Hour
- Minute
- Second
- Delta Days
- Delta Hours
- Delta Minutes
- Delta Seconds
- Reset Time
- Set From OSV
- Set From TLE
- Caption
- Target Name
- Local Time
- UTC Time
- Julian Time
- Sun Right Ascension
- Sun Declination
- Sun Longitude
- Sun Latitude
- Moon Right Ascension
- Moon Declination
- Moon Longitude
- Moon Latitude
- Telemetry
- OSV J2000
- OSV ECEF
- Geodetic Coordinates
- Osculating Elements
- Two-Line Element
- Export TLE
- Fill from OSV
- Satellite Name
- Launch Year
- Launch Number
- Piece of Launch
- Epoch Year
- Epoch Day
- Mean Motion 1st Der
- The drag term
- Element Set Number
- Catalog Number
- Inclination
- RA of Asc. Node
- Eccentricity
- Argument of Perigee
- Mean Anomaly
- Mean Motion
- Revolution Number
- Orbit State Vector
- OSV Year
- OSV Month
- OSV Day
- OSV Hour
- OSV Minute
- OSV Second
- X (km)
- Y (km)
- Z (km)
- Vx (m/s)
- Vy (m/s)
- Vz (m/s)
- Keplerian Elements
- Override
- Eccentricity
- Semimajor Axis
- Inclination
- Long. Asc. Node
- Arg. Perigee
- Mean Anomaly
GitHub

Close Controls