STARLINK-32623, 62152

Orbit data source: Space-Track

STARLINK-32623, 62152 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 30 Nov 2024 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
62152, 2024-224P
Orbit
LEO
Last TLE update
16 hours ago
Origin
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
2024-11-30 (8 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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago
0 STARLINK-32623
1 62152U 24224P   25218.58082936  .00025436  00000-0  92965-3 0  9993
2 62152  42.9992 296.2383 0000826 266.4023  93.6734 15.27615848 39488
Epoch: 2025-08-06T13:56Z
TLE epoch observation values (Epoch: 2025-08-06T13:56:23.656Z)
Latitude
-0.00004°
Longitude
131.78215°
Altitude
482.753 km
Speed
7.626 km/s
True Right ascension
19h 44m 57s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
1.48004°
Longitude
-53.67369°
Altitude
482.462 km
Speed
7.626 km/s
Apparent Right ascension
07h 50m 08s
Apparent Declination
-18° 29' 47"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
20:28:03
Azimuth
23.632° NE
Elevation
-67.073°
Doppler factor
1
Orbital elements
Apogee altitude
485.454 km
Perigee altitude
484.32 km
Semi-major axis
6,863.024 km
Eccentricity
0.00008
Inclination
42.9992°
RAAN
296.2383°
Arg. of periapsis
266.4023°
True anomaly
93.68285°
Mean anomaly
93.6734°
Eccentric anomaly
93.67812°
Mean motion
3.81742 °/min
Orbital period
94.3 mins
BSTAR
0.00092965
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
|