Showing default

IRIDIUM 138, 43071

Orbit data source: Space-Track

IRIDIUM 138, 43071 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
43071, 2017-083B
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: 15 hours ago

TLE from 15 hours ago
0 IRIDIUM 138
1 43071U 17083B   25363.49989685  .00000132  00000-0  40099-4 0  9993
2 43071  86.3970  32.6044 0001905 100.6904 259.4507 14.34218075419814
Epoch: 2025-12-29T11:59Z
TLE epoch observation values (Epoch: 2025-12-29T11:59:51.087Z)
Latitude
0.00002°
Longitude
114.4449°
Altitude
780.967 km
Speed
7.463 km/s
True Right ascension
02h 10m 25s
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
03:03:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.993 km
Perigee altitude
773.268 km
Semi-major axis
7,152.768 km
Eccentricity
0.00019
Inclination
86.397°
RAAN
32.6044°
Arg. of periapsis
100.6904°
True anomaly
259.42924°
Mean anomaly
259.4507°
Eccentric anomaly
259.43997°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000040099
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
|