IRIDIUM 152, 43479
Orbit data source: Space-Track
IRIDIUM 152, 43479 is a payload satellite owned by Iridium (US) in LEO that was launched on Tue, 22 May 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.
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43479 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 IRIDIUM 152
1 43479U 18047D 25314.86590238 .00000122 00000-0 36603-4 0 9990
2 43479 86.4008 179.5479 0002115 82.4998 277.6438 14.34219221391195Epoch: 2025-11-10T20:46Z
TLE epoch observation values (Epoch: 2025-11-10T20:46:53.965Z)
Latitude
-0.00004°
Longitude
177.56237°
Altitude
780.512 km
Speed
7.464 km/s
True Right ascension
11h 58m 11s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:13:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.139 km
Perigee altitude
773.114 km
Semi-major axis
7,152.764 km
Eccentricity
0.00021
Inclination
86.4008°
RAAN
179.5479°
Arg. of periapsis
82.4998°
True anomaly
277.61978°
Mean anomaly
277.6438°
Eccentric anomaly
277.63179°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000036603
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Other satellites on launch #47 in the year 2018 (2018-05-22 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 152 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-11 15:18:09.824Z | 164.473° S | 2025-11-11 15:23:09.824Z | 88.143° E | 39.337° | 2025-11-11 15:28:09.824Z | 11.859° NNE |
| 5 mins | 2025-11-11 17:02:09.824Z | 257.873° W | 2025-11-11 17:04:09.824Z | 283.728° WNW | 15.625° | 2025-11-11 17:07:09.824Z | 320.59° NNW |
| 8 mins | 2025-11-12 03:31:09.824Z | 345.484° N | 2025-11-12 03:34:09.824Z | 281.52° WNW | 41.745° | 2025-11-12 03:39:09.824Z | 191.314° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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