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, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 IRIDIUM 116
1 43072U 17083C   26037.39901707  .00000337  00000-0  11313-3 0  9994
2 43072  86.3973  16.6520 0001906  81.9430 278.1982 14.34217615425423
Epoch: 2026-02-06T09:34Z
TLE epoch observation values (Epoch: 2026-02-06T09:34:35.074Z)
Latitude
-0.00005°
Longitude
96.4684°
Altitude
780.524 km
Speed
7.464 km/s
True Right ascension
01h 06m 36s
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
22:42:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.995 km
Perigee altitude
773.269 km
Semi-major axis
7,152.769 km
Eccentricity
0.00019
Inclination
86.3973°
RAAN
16.652°
Arg. of periapsis
81.943°
True anomaly
278.17658°
Mean anomaly
278.1982°
Eccentric anomaly
278.18739°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00011313
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
|