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 (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: 13 hours ago

TLE from 13 hours ago
0 IRIDIUM 170
1 43930U 19002J   26252.58106952  .00000455  00000-0  68229-4 0  9999
2 43930  86.6110 318.2734 0002468  95.2717 264.8781 14.72253184411674
Epoch: 2026-09-09T13:56Z
TLE epoch observation values (Epoch: 2026-09-09T13:56:44.406Z)
Latitude
-0.00011°
Longitude
120.45729°
Altitude
657.147 km
Speed
7.529 km/s
True Right ascension
21h 13m 05s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
18:51:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.526 km
Perigee altitude
649.056 km
Semi-major axis
7,028.928 km
Eccentricity
0.00025
Inclination
86.611°
RAAN
318.2734°
Arg. of periapsis
95.2717°
True anomaly
264.84993°
Mean anomaly
264.8781°
Eccentric anomaly
264.86402°
Mean motion
3.68307 °/min
Orbital period
97.74 mins
BSTAR
0.000068229
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
|