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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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: 10 hours ago
TLE from 10 hours ago
0 IRIDIUM 162
1 43482U 18047G 25315.18652897 .00000649 00000-0 18697-3 0 9996
2 43482 86.4531 179.4473 0002019 78.3241 281.8186 14.43284493393687Epoch: 2025-11-11T04:28Z
TLE epoch observation values (Epoch: 2025-11-11T04:28:36.103Z)
Latitude
-0.00004°
Longitude
61.72017°
Altitude
750.437 km
Speed
7.479 km/s
True Right ascension
11h 57m 47s
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
10:28:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.056 km
Perigee altitude
743.18 km
Semi-major axis
7,122.755 km
Eccentricity
0.0002
Inclination
86.4531°
RAAN
179.4473°
Arg. of periapsis
78.3241°
True anomaly
281.79595°
Mean anomaly
281.8186°
Eccentric anomaly
281.80728°
Mean motion
3.61053 °/min
Orbital period
99.71 mins
BSTAR
0.00018697
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-11 14:35:46.775Z | 122.669° SE | 2025-11-11 14:38:46.775Z | 82.971° E | 18.838° | 2025-11-11 14:41:46.775Z | 41.51° NE |
| 7 mins | 2025-11-11 16:15:46.775Z | 218.154° SW | 2025-11-11 16:18:46.775Z | 281.248° WNW | 33.5° | 2025-11-11 16:22:46.775Z | 344.855° N |
| 8 mins | 2025-11-12 02:41:46.775Z | 20.318° NNE | 2025-11-12 02:44:46.775Z | 72.391° E | 33.188° | 2025-11-12 02:49:46.775Z | 153.19° SSE |
| 5 mins | 2025-11-12 04:22:46.775Z | 309.77° NW | 2025-11-12 04:24:46.775Z | 280.324° WNW | 18.926° | 2025-11-12 04:27:46.775Z | 239.167° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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