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 (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: 9 hours ago

TLE from 9 hours ago
0 IRIDIUM 169
1 43926U 19002E   26306.45955304  .00000123  00000-0  33732-4 0  9996
2 43926  86.4216 327.4193 0002066  99.7131 260.4300 14.38607330410102
Epoch: 2026-11-02T11:01Z
TLE epoch observation values (Epoch: 2026-11-02T11:01:45.382Z)
Latitude
-0.00011°
Longitude
120.24394°
Altitude
766.407 km
Speed
7.471 km/s
True Right ascension
21h 49m 40s
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
15:37:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
761.536 km
Perigee altitude
758.587 km
Semi-major axis
7,138.198 km
Eccentricity
0.00021
Inclination
86.4216°
RAAN
327.4193°
Arg. of periapsis
99.7131°
True anomaly
260.40666°
Mean anomaly
260.43°
Eccentric anomaly
260.41833°
Mean motion
3.59882 °/min
Orbital period
100.03 mins
BSTAR
0.000033732
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
|