DECAYED

STARLINK-5092, 55408 (Decayed)

Orbit data source: Space-Track

STARLINK-5092, 55408 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 31 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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.

Not visible in the next 10 days
Identifier
55408, 2023-014T
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Decayed Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
305 kg wet, ~290 kg dry
Launch date (UTC)
2023-01-31 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
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: 3 months ago

TLE from 3 months ago
0 STARLINK-5092
1 55408U 23014T   26083.28502045  .12725752  45178-5  17770-3 0  9993
2 55408  69.9922   8.0114 0006728 234.9391 125.1214 16.48782581174726
Epoch: 2026-03-24T06:50Z
TLE epoch observation values (Epoch: 2026-03-24T06:50:25.766Z)
Latitude
-0.00005°
Longitude
83.63915°
Altitude
147.653 km
Speed
7.816 km/s
True Right ascension
00h 32m 02s
True Declination
0° 00' 00"
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
21:30:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
144.743 km
Perigee altitude
135.971 km
Semi-major axis
6,518.494 km
Eccentricity
0.00067
Inclination
69.9922°
RAAN
8.0114°
Arg. of periapsis
234.9391°
True anomaly
125.18443°
Mean anomaly
125.1214°
Eccentric anomaly
125.15292°
Mean motion
4.12403 °/min
Orbital period
87.29 mins
BSTAR
0.0001777
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|