STARLINK-5672, 55468

Orbit data source: Space-Track

STARLINK-5672, 55468 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Feb 2023 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
55468, 2023-015V
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
305 kg wet, ~290 kg dry
Launch date (UTC)
2023-02-02 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 STARLINK-5672
1 55468U 23015V   26083.91667824  .00129822  00000-0  60780-2 0  9998
2 55468  42.9992 242.1683 0001035 301.6062 189.0733 15.18505448  5779
Epoch: 2026-03-24T22:00Z
TLE epoch observation values (Epoch: 2026-03-24T22:00:00.999Z)
Latitude
31.26322°
Longitude
-130.57682°
Altitude
511.849 km
Speed
7.612 km/s
True Right ascension
01h 27m 15s
True Declination
31° 06' 20"
Sunlit
Object was in daylight 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
10:59:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.008 km
Perigee altitude
511.581 km
Semi-major axis
6,890.431 km
Eccentricity
0.0001
Inclination
42.9992°
RAAN
242.1683°
Arg. of periapsis
301.6062°
True anomaly
189.07143°
Mean anomaly
189.0733°
Eccentric anomaly
189.07236°
Mean motion
3.79467 °/min
Orbital period
94.87 mins
BSTAR
0.006078
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|