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IRIDIUM 165, 43572

Orbit data source: Space-Track

IRIDIUM 165, 43572 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
43572, 2018-061D
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: 12 hours ago

TLE from 12 hours ago
0 IRIDIUM 165
1 43572U 18061D   26051.63572300  .00000001  00000-0 -66752-5 0  9990
2 43572  86.3941 105.5574 0001978  97.7501 262.3920 14.34217576396681
Epoch: 2026-02-20T15:15Z
TLE epoch observation values (Epoch: 2026-02-20T15:15:26.467Z)
Latitude
0.00005°
Longitude
86.1273°
Altitude
780.906 km
Speed
7.463 km/s
True Right ascension
07h 02m 13s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
06:15:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.047 km
Perigee altitude
773.217 km
Semi-major axis
7,152.769 km
Eccentricity
0.0002
Inclination
86.3941°
RAAN
105.5574°
Arg. of periapsis
97.7501°
True anomaly
262.36953°
Mean anomaly
262.392°
Eccentric anomaly
262.38077°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000066752
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Documentation

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