Showing default

IRIDIUM 153, 43078

Orbit data source: Space-Track

IRIDIUM 153, 43078 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
43078, 2017-083J
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: 7 hours ago

TLE from 7 hours ago
0 IRIDIUM 153
1 43078U 17083J   26168.78240115  .00000027  00000-0  27550-5 0  9995
2 43078  86.3961 290.2219 0002245  89.7741 270.3712 14.34217611445365
Epoch: 2026-06-17T18:46Z
TLE epoch observation values (Epoch: 2026-06-17T18:46:39.459Z)
Latitude
-0.00002°
Longitude
102.52234°
Altitude
780.708 km
Speed
7.463 km/s
True Right ascension
19h 20m 53s
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
12:33:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.238 km
Perigee altitude
773.026 km
Semi-major axis
7,152.769 km
Eccentricity
0.00022
Inclination
86.3961°
RAAN
290.2219°
Arg. of periapsis
89.7741°
True anomaly
270.34547°
Mean anomaly
270.3712°
Eccentric anomaly
270.35834°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000002755
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
|