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IRIDIUM 156, 43576

Orbit data source: Space-Track

IRIDIUM 156, 43576 is a payload satellite owned by Iridium (US) in LEO that was launched on Wed, 25 Jul 2018 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
43576, 2018-061H
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NGIS SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
2018-07-25 (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, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 IRIDIUM 156
1 43576U 18061H   26171.39656089  .00000206  00000-0  66320-4 0  9993
2 43576  86.3959  55.3875 0002040  83.6900 276.4528 14.34216473413830
Epoch: 2026-06-20T09:31Z
TLE epoch observation values (Epoch: 2026-06-20T09:31:02.860Z)
Latitude
-0.00006°
Longitude
4.0138°
Altitude
780.559 km
Speed
7.464 km/s
True Right ascension
03h 41m 32s
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
00:50:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.095 km
Perigee altitude
773.177 km
Semi-major axis
7,152.773 km
Eccentricity
0.0002
Inclination
86.3959°
RAAN
55.3875°
Arg. of periapsis
83.69°
True anomaly
276.42957°
Mean anomaly
276.4528°
Eccentric anomaly
276.44119°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00006632
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