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IRIDIUM 142, 43256

Orbit data source: Space-Track

IRIDIUM 142, 43256 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 30 Mar 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
43256, 2018-030H
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)
2018-03-30 (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: 8 hours ago

TLE from 8 hours ago
0 IRIDIUM 142
1 43256U 18030H   26131.41185730  .00000055  00000-0  12747-4 0  9999
2 43256  86.3930 305.7362 0002102  84.5568 275.5868 14.34218807424861
Epoch: 2026-05-11T09:53Z
TLE epoch observation values (Epoch: 2026-05-11T09:53:04.470Z)
Latitude
0.00001°
Longitude
-71.73339°
Altitude
780.568 km
Speed
7.464 km/s
True Right ascension
20h 22m 56s
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
02:15:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.132 km
Perigee altitude
773.125 km
Semi-major axis
7,152.765 km
Eccentricity
0.00021
Inclination
86.393°
RAAN
305.7362°
Arg. of periapsis
84.5568°
True anomaly
275.56283°
Mean anomaly
275.5868°
Eccentric anomaly
275.57481°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000012747
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Documentation

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