STARLINK-36438, 67625

Orbit data source: Space-Track

STARLINK-36438, 67625 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 30 Jan 2026 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
67625, 2026-020J
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
2026-01-30 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 STARLINK-36438
1 67625U 26020J   26171.35016462  .00014568  00000-0  53767-3 0  9995
2 67625  42.9996 280.0605 0001126 251.3648 108.7081 15.27592226 21815
Epoch: 2026-06-20T08:24Z
TLE epoch observation values (Epoch: 2026-06-20T08:24:14.223Z)
Latitude
-0.00003°
Longitude
-114.56485°
Altitude
483.036 km
Speed
7.626 km/s
True Right ascension
18h 40m 14s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.731 km
Perigee altitude
484.185 km
Semi-major axis
6,863.095 km
Eccentricity
0.00011
Inclination
42.9996°
RAAN
280.0605°
Arg. of periapsis
251.3648°
True anomaly
108.72032°
Mean anomaly
108.7081°
Eccentric anomaly
108.71421°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.00053767
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|