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: 7 hours ago
TLE from 7 hours ago
0 IRIDIUM 134
1 43075U 17083F 25312.72744243 .00000264 00000-0 87038-4 0 9996
2 43075 86.3983 54.2055 0001820 95.3866 264.7537 14.34219390412509Epoch: 2025-11-08T17:27Z
TLE epoch observation values (Epoch: 2025-11-08T17:27:31.025Z)
Latitude
-0.0001°
Longitude
104.17332°
Altitude
780.832 km
Speed
7.463 km/s
True Right ascension
03h 36m 49s
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
20:26:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.928 km
Perigee altitude
773.324 km
Semi-major axis
7,152.763 km
Eccentricity
0.00018
Inclination
86.3983°
RAAN
54.2055°
Arg. of periapsis
95.3866°
True anomaly
264.73293°
Mean anomaly
264.7537°
Eccentric anomaly
264.74332°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000087038
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-09 06:57:54.206Z | 156.221° SSE | 2025-11-09 07:02:54.206Z | 70.047° E | 34.505° | 2025-11-09 07:06:54.206Z | 17.197° NNE |
| 6 mins | 2025-11-09 08:40:54.206Z | 249.336° W | 2025-11-09 08:42:54.206Z | 276.472° WNW | 18.502° | 2025-11-09 08:46:54.206Z | 328.177° NNW |
| 8 mins | 2025-11-09 19:09:54.206Z | 353.135° N | 2025-11-09 19:13:54.206Z | 225.578° WSW | 43.784° | 2025-11-09 19:17:54.206Z | 184.867° 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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