IRIDIUM 134, 43075
Orbit data source: Space-Track
IRIDIUM 134, 43075 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.
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43075 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: 11 hours ago
TLE from 11 hours ago
0 IRIDIUM 134
1 43075U 17083F 25302.82031373 .00000389 00000-0 13183-3 0 9996
2 43075 86.3971 58.3457 0001856 90.0579 270.0829 14.34218647411089Epoch: 2025-10-29T19:41Z
TLE epoch observation values (Epoch: 2025-10-29T19:41:15.106Z)
Latitude
-0.00006°
Longitude
84.64479°
Altitude
780.713 km
Speed
7.463 km/s
True Right ascension
03h 53m 22s
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
02:28:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.956 km
Perigee altitude
773.301 km
Semi-major axis
7,152.766 km
Eccentricity
0.00019
Inclination
86.3971°
RAAN
58.3457°
Arg. of periapsis
90.0579°
True anomaly
270.06163°
Mean anomaly
270.0829°
Eccentric anomaly
270.07227°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00013183
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Other satellites on launch #83 in the year 2017 (2017-12-23 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 134 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-30 07:32:14.947Z | 134.026° SE | 2025-10-30 07:36:14.947Z | 73.776° E | 24.356° | 2025-10-30 07:39:14.947Z | 32.532° NE |
| 7 mins | 2025-10-30 09:13:14.947Z | 227.416° WSW | 2025-10-30 09:16:14.947Z | 276.817° WNW | 27.767° | 2025-10-30 09:20:14.947Z | 337.647° N |
| 8 mins | 2025-10-30 19:43:14.947Z | 8.581° NNE | 2025-10-30 19:47:14.947Z | 115.679° SE | 40.991° | 2025-10-30 19:51:14.947Z | 166.035° S |
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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