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IRIDIUM 138, 43071

Orbit data source: Space-Track

IRIDIUM 138, 43071 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
43071, 2017-083B
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 138
1 43071U 17083B   25243.07943303  .00000008  00000-0 -42960-5 0  9994
2 43071  86.3895  82.9605 0001490  88.4695 271.6671 14.34217529402554
Epoch: 2025-08-31T01:54Z
TLE epoch observation values (Epoch: 2025-08-31T01:54:23.013Z)
Latitude
-0.00009°
Longitude
74.86008°
Altitude
780.688 km
Speed
7.464 km/s
True Right ascension
05h 31m 50s
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
08:00:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.698 km
Perigee altitude
773.567 km
Semi-major axis
7,152.77 km
Eccentricity
0.00015
Inclination
86.3895°
RAAN
82.9605°
Arg. of periapsis
88.4695°
True anomaly
271.65003°
Mean anomaly
271.6671°
Eccentric anomaly
271.65857°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000004296
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