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IRIDIUM 134, 43075

Orbit data source: Space-Track

IRIDIUM 134, 43075 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 23 Dec 2017 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.

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Identifier
43075, 2017-083F
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
2017-12-23 (8 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 IRIDIUM 134
1 43075U 17083F   25243.09846180  .00000080  00000-0  21360-4 0  9994
2 43075  86.3912  83.3367 0002315  93.3946 266.7515 14.34217801402521
Epoch: 2025-08-31T02:21Z
TLE epoch observation values (Epoch: 2025-08-31T02:21:47.099Z)
Latitude
0.00001°
Longitude
68.36717°
Altitude
780.812 km
Speed
7.463 km/s
True Right ascension
05h 33m 20s
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
07:59:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.287 km
Perigee altitude
772.976 km
Semi-major axis
7,152.769 km
Eccentricity
0.00023
Inclination
86.3912°
RAAN
83.3367°
Arg. of periapsis
93.3946°
True anomaly
266.72502°
Mean anomaly
266.7515°
Eccentric anomaly
266.73826°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00002136
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