IRIDIUM 162, 43482
Orbit data source: Space-Track
IRIDIUM 162, 43482 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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43482 intel report (Beta)
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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: 11 hours ago
TLE from 11 hours ago
0 IRIDIUM 162
1 43482U 18047G 26091.13610694 .00000287 00000-0 79362-4 0 9997
2 43482 86.4452 120.5910 0002247 95.2101 264.9357 14.43275548414012Epoch: 2026-04-01T03:15Z
TLE epoch observation values (Epoch: 2026-04-01T03:15:59.639Z)
Latitude
0.00003°
Longitude
-117.91077°
Altitude
750.903 km
Speed
7.479 km/s
True Right ascension
08h 02m 21s
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
19:41:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.248 km
Perigee altitude
743.047 km
Semi-major axis
7,122.784 km
Eccentricity
0.00022
Inclination
86.4452°
RAAN
120.591°
Arg. of periapsis
95.2101°
True anomaly
264.91005°
Mean anomaly
264.9357°
Eccentric anomaly
264.92288°
Mean motion
3.61051 °/min
Orbital period
99.71 mins
BSTAR
0.000079362
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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 162 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-01 15:31:11.586Z | 307.004° NW | 2026-04-01 15:33:11.586Z | 282.435° WNW | 13.262° | 2026-04-01 15:35:11.586Z | 257.705° W |
| 8 mins | 2026-04-02 02:41:11.586Z | 194.364° SSW | 2026-04-02 02:45:11.586Z | 302.234° NW | 41.846° | 2026-04-02 02:49:11.586Z | 355.432° N |
| 7 mins | 2026-04-02 13:08:11.586Z | 32.111° NE | 2026-04-02 13:11:11.586Z | 79.389° E | 24.221° | 2026-04-02 13:15:11.586Z | 135.35° SSE |
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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