IRIDIUM 138, 43071
Orbit data source: Space-Track
IRIDIUM 138, 43071 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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43071 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: 8 hours ago
TLE from 8 hours ago
0 IRIDIUM 138
1 43071U 17083B 26192.80522216 .00000111 00000-0 32464-4 0 9996
2 43071 86.3996 311.4236 0002064 91.9039 268.2394 14.34217698447667Epoch: 2026-07-11T19:19Z
TLE epoch observation values (Epoch: 2026-07-11T19:19:31.194Z)
Latitude
0.00005°
Longitude
91.83046°
Altitude
780.764 km
Speed
7.463 km/s
True Right ascension
20h 45m 41s
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
16:00:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.108 km
Perigee altitude
773.155 km
Semi-major axis
7,152.769 km
Eccentricity
0.00021
Inclination
86.3996°
RAAN
311.4236°
Arg. of periapsis
91.9039°
True anomaly
268.21576°
Mean anomaly
268.2394°
Eccentric anomaly
268.22758°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000032464
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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 138 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-12 07:11:56.946Z | 106.762° ESE | 2026-07-12 07:13:56.946Z | 82.921° E | 14.135° | 2026-07-12 07:16:56.946Z | 46.85° ENE |
| 8 mins | 2026-07-12 08:50:56.946Z | 199.453° SSW | 2026-07-12 08:53:56.946Z | 247.925° W | 40.123° | 2026-07-12 08:58:56.946Z | 353.458° N |
| 7 mins | 2026-07-12 19:21:56.946Z | 29.7° NE | 2026-07-12 19:24:56.946Z | 83.39° E | 28.846° | 2026-07-12 19:28:56.946Z | 142.032° SSE |
| 6 mins | 2026-07-12 21:02:56.946Z | 316.654° NNW | 2026-07-12 21:04:56.946Z | 285.8° WNW | 23.408° | 2026-07-12 21:08:56.946Z | 227.354° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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