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IRIDIUM 109, 41919

Orbit data source: Space-Track

IRIDIUM 109, 41919 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 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
41919, 2017-003C
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)
2017-01-14 (10 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: 14 hours ago

TLE from 14 hours ago
0 IRIDIUM 109
1 41919U 17003C   26233.46225118  .00000056  00000-0  12842-4 0  9992
2 41919  86.3916  61.2063 0002192  90.4000 269.7447 14.34217562502555
Epoch: 2026-08-21T11:05Z
TLE epoch observation values (Epoch: 2026-08-21T11:05:38.501Z)
Latitude
-0.00005°
Longitude
-74.99079°
Altitude
780.726 km
Speed
7.463 km/s
True Right ascension
04h 04m 49s
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
15:57:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.2 km
Perigee altitude
773.064 km
Semi-major axis
7,152.769 km
Eccentricity
0.00022
Inclination
86.3916°
RAAN
61.2063°
Arg. of periapsis
90.4°
True anomaly
269.71958°
Mean anomaly
269.7447°
Eccentric anomaly
269.73214°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000012842
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