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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 (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 169
1 43926U 19002E   26303.32954011  .00000151  00000-0  42770-4 0  9996
2 43926  86.4218 328.7282 0002059  99.0326 261.1106 14.38606874409650
Epoch: 2026-10-30T07:54Z
TLE epoch observation values (Epoch: 2026-10-30T07:54:32.265Z)
Latitude
0.00004°
Longitude
171.44259°
Altitude
766.39 km
Speed
7.471 km/s
True Right ascension
21h 54m 54s
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
15:14:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
761.533 km
Perigee altitude
758.593 km
Semi-major axis
7,138.2 km
Eccentricity
0.00021
Inclination
86.4218°
RAAN
328.7282°
Arg. of periapsis
99.0326°
True anomaly
261.08729°
Mean anomaly
261.1106°
Eccentric anomaly
261.09894°
Mean motion
3.59882 °/min
Orbital period
100.03 mins
BSTAR
0.00004277
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