Showing default

IRIDIUM 116, 43072

Orbit data source: Space-Track

IRIDIUM 116, 43072 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 23 Dec 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.

Loading next visibility...
Identifier
43072, 2017-083C
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)
2017-12-23 (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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 IRIDIUM 116
1 43072U 17083C   25243.25702606  .00000123  00000-0  36801-4 0  9997
2 43072  86.3908  83.2150 0002363  87.9456 272.2010 14.34217955402612
Epoch: 2025-08-31T06:10Z
TLE epoch observation values (Epoch: 2025-08-31T06:10:07.051Z)
Latitude
-0.00007°
Longitude
11.00605°
Altitude
780.653 km
Speed
7.464 km/s
True Right ascension
05h 32m 51s
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
07:59:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.321 km
Perigee altitude
772.941 km
Semi-major axis
7,152.768 km
Eccentricity
0.00024
Inclination
86.3908°
RAAN
83.215°
Arg. of periapsis
87.9456°
True anomaly
272.17394°
Mean anomaly
272.201°
Eccentric anomaly
272.18747°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000036801
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
|