Showing default

IRIDIUM 150, 43257

Orbit data source: Space-Track

IRIDIUM 150, 43257 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 30 Mar 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
43257, 2018-030J
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)
2018-03-30 (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: 14 hours ago

TLE from 14 hours ago
0 IRIDIUM 150
1 43257U 18030J   25340.09864786  .00000232  00000-0  75810-4 0  9997
2 43257  86.3978  11.1852 0002269  96.9960 263.1494 14.34219947402481
Epoch: 2025-12-06T02:22Z
TLE epoch observation values (Epoch: 2025-12-06T02:22:03.175Z)
Latitude
0.00001°
Longitude
-99.45929°
Altitude
780.905 km
Speed
7.463 km/s
True Right ascension
00h 44m 44s
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
14:29:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.247 km
Perigee altitude
773.001 km
Semi-major axis
7,152.761 km
Eccentricity
0.00023
Inclination
86.3978°
RAAN
11.1852°
Arg. of periapsis
96.996°
True anomaly
263.12359°
Mean anomaly
263.1494°
Eccentric anomaly
263.13649°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.00007581
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
|