Showing default

IRIDIUM 170, 43930

Orbit data source: Space-Track

IRIDIUM 170, 43930 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
43930, 2019-002J
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: 9 hours ago

TLE from 9 hours ago
0 IRIDIUM 170
1 43930U 19002J   26125.41348235  .00000825  00000-0  12688-3 0  9990
2 43930  86.6126  11.4279 0002288  87.4700 272.6779 14.72252486392960
Epoch: 2026-05-05T09:55Z
TLE epoch observation values (Epoch: 2026-05-05T09:55:24.875Z)
Latitude
-0°
Longitude
-0.71443°
Altitude
656.919 km
Speed
7.529 km/s
True Right ascension
00h 45m 42s
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
02:36:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.401 km
Perigee altitude
649.185 km
Semi-major axis
7,028.93 km
Eccentricity
0.00023
Inclination
86.6126°
RAAN
11.4279°
Arg. of periapsis
87.47°
True anomaly
272.65171°
Mean anomaly
272.6779°
Eccentric anomaly
272.6648°
Mean motion
3.68306 °/min
Orbital period
97.74 mins
BSTAR
0.00012688
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
|