Showing default

IRIDIUM 155, 43573

Orbit data source: Space-Track

IRIDIUM 155, 43573 is a payload satellite owned by Iridium (US) in LEO that was launched on Wed, 25 Jul 2018 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
43573, 2018-061E
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)
2018-07-25 (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: 11 hours ago

TLE from 11 hours ago
0 IRIDIUM 155
1 43573U 18061E   25351.29433527 -.00000008  00000-0 -97635-5 0  9994
2 43573  86.3976 132.7334 0001990  99.7384 260.4037 14.34217078387282
Epoch: 2025-12-17T07:03Z
TLE epoch observation values (Epoch: 2025-12-17T07:03:50.567Z)
Latitude
0.00002°
Longitude
-59.39355°
Altitude
780.958 km
Speed
7.463 km/s
True Right ascension
08h 50m 56s
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
16:45:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.057 km
Perigee altitude
773.21 km
Semi-major axis
7,152.771 km
Eccentricity
0.0002
Inclination
86.3976°
RAAN
132.7334°
Arg. of periapsis
99.7384°
True anomaly
260.38122°
Mean anomaly
260.4037°
Eccentric anomaly
260.39246°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000097635
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
|