IRIDIUM 132, 42961
Orbit data source: Space-Track
IRIDIUM 132, 42961 is a payload satellite owned by Iridium (US) in LEO that was launched on Mon, 09 Oct 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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42961 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 132
1 42961U 17061G 26107.17438303 .00000144 00000-0 44505-4 0 9993
2 42961 86.3978 50.7453 0002283 86.8941 273.2516 14.34217629446076Epoch: 2026-04-17T04:11Z
TLE epoch observation values (Epoch: 2026-04-17T04:11:06.693Z)
Latitude
-0.00004°
Longitude
142.65605°
Altitude
780.626 km
Speed
7.464 km/s
True Right ascension
03h 22m 58s
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
22:01:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.265 km
Perigee altitude
772.999 km
Semi-major axis
7,152.769 km
Eccentricity
0.00023
Inclination
86.3978°
RAAN
50.7453°
Arg. of periapsis
86.8941°
True anomaly
273.22548°
Mean anomaly
273.2516°
Eccentric anomaly
273.23854°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000044505
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Other satellites on launch #61 in the year 2017 (2017-10-09 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 132 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 | 2026-04-17 19:24:28.803Z | 106.175° ESE | 2026-04-17 19:26:28.803Z | 82.714° E | 13.642° | 2026-04-17 19:28:28.803Z | 57.72° ENE |
| 8 mins | 2026-04-17 21:03:28.803Z | 197.96° SSW | 2026-04-17 21:06:28.803Z | 246.17° WSW | 40.746° | 2026-04-17 21:11:28.803Z | 354.253° N |
| 7 mins | 2026-04-18 07:34:28.803Z | 30.622° NE | 2026-04-18 07:37:28.803Z | 83.543° E | 28.122° | 2026-04-18 07:41:28.803Z | 141.045° SSE |
| 6 mins | 2026-04-18 09:15:28.803Z | 317.215° NNW | 2026-04-18 09:17:28.803Z | 285.838° WNW | 24.051° | 2026-04-18 09:21:28.803Z | 226.343° 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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