Showing default

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.

Loading next visibility...
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: 13 hours ago

TLE from 13 hours ago
0 IRIDIUM 169
1 43926U 19002E   25293.49350150  .00000219  00000-0  65021-4 0  9994
2 43926  86.4196 125.4240 0002864  63.3996 296.7495 14.38608511355769
Epoch: 2025-10-20T11:50Z
TLE epoch observation values (Epoch: 2025-10-20T11:50:38.529Z)
Latitude
-0.00008°
Longitude
-81.43156°
Altitude
765.237 km
Speed
7.472 km/s
True Right ascension
08h 21m 41s
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
19:26:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
762.102 km
Perigee altitude
758.013 km
Semi-major axis
7,138.194 km
Eccentricity
0.00029
Inclination
86.4196°
RAAN
125.424°
Arg. of periapsis
63.3996°
True anomaly
296.72019°
Mean anomaly
296.7495°
Eccentric anomaly
296.73484°
Mean motion
3.59882 °/min
Orbital period
100.03 mins
BSTAR
0.000065021
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|