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IRIDIUM 169, 43926

Orbit data source: Space-Track

IRIDIUM 169, 43926 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 11 Jan 2019 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
43926, 2019-002E
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)
2019-01-11 (7 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: 7 hours ago

TLE from 7 hours ago
0 IRIDIUM 169
1 43926U 19002E   26036.51361483  .00000389  00000-0  12081-3 0  9999
2 43926  86.4177  80.2581 0002737  76.4826 283.6678 14.38611169371297
Epoch: 2026-02-05T12:19Z
TLE epoch observation values (Epoch: 2026-02-05T12:19:36.321Z)
Latitude
0.00008°
Longitude
119.69201°
Altitude
765.687 km
Speed
7.472 km/s
True Right ascension
05h 21m 01s
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
21:52:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
762.002 km
Perigee altitude
758.095 km
Semi-major axis
7,138.186 km
Eccentricity
0.00027
Inclination
86.4177°
RAAN
80.2581°
Arg. of periapsis
76.4826°
True anomaly
283.63732°
Mean anomaly
283.6678°
Eccentric anomaly
283.65256°
Mean motion
3.59883 °/min
Orbital period
100.03 mins
BSTAR
0.00012081
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Documentation

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