STARLINK-1169, 45061

Orbit data source: Space-Track

STARLINK-1169, 45061 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 29 Jan 2020 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
45061, 2020-006T
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Partially operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
260 kg wet, ~248 kg dry
Launch date (UTC)
2020-01-29 (7 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: 22 hours ago

TLE from 22 hours ago
0 STARLINK-1169
1 45061U 20006T   26262.00313860  .00048001  00000-0  90005-3 0  9993
2 45061  53.1501  91.0240 0001996 197.8855 162.2084 15.48197721366314
Epoch: 2026-09-19T00:04Z
TLE epoch observation values (Epoch: 2026-09-19T00:04:31.175Z)
Latitude
0.00004°
Longitude
91.97622°
Altitude
424.196 km
Speed
7.657 km/s
True Right ascension
06h 04m 05s
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
15:21:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
423.616 km
Perigee altitude
420.901 km
Semi-major axis
6,800.395 km
Eccentricity
0.0002
Inclination
53.1501°
RAAN
91.024°
Arg. of periapsis
197.8855°
True anomaly
162.21539°
Mean anomaly
162.2084°
Eccentric anomaly
162.21189°
Mean motion
3.87028 °/min
Orbital period
93.02 mins
BSTAR
0.00090005
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|