STARLINK-33623, 63072

Orbit data source: Space-Track

STARLINK-33623, 63072 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 21 Feb 2025 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
63072, 2025-035W
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)
2025-02-21 (1 year 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: 11 hours ago

TLE from 11 hours ago
0 STARLINK-33623
1 63072U 25035W   26171.39546399  .00024826  00000-0  90837-3 0  9990
2 63072  42.9988 287.3641 0001736 273.5001  86.5652 15.27589173 75435
Epoch: 2026-06-20T09:29Z
TLE epoch observation values (Epoch: 2026-06-20T09:29:28.088Z)
Latitude
-0.00003°
Longitude
-123.61367°
Altitude
482.726 km
Speed
7.626 km/s
True Right ascension
19h 09m 27s
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
07:17:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.158 km
Perigee altitude
483.776 km
Semi-major axis
6,863.104 km
Eccentricity
0.00017
Inclination
42.9988°
RAAN
287.3641°
Arg. of periapsis
273.5001°
True anomaly
86.58506°
Mean anomaly
86.5652°
Eccentric anomaly
86.57513°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.00090837
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
|