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: 6 hours ago
TLE from 6 hours ago
0 IRIDIUM 132
1 42961U 17061G 26141.77956191 .00000176 00000-0 55720-4 0 9993
2 42961 86.3991 36.2880 0002281 85.2886 274.8570 14.34216588451035Epoch: 2026-05-21T18:42Z
TLE epoch observation values (Epoch: 2026-05-21T18:42:34.149Z)
Latitude
-0.00002°
Longitude
-123.77415°
Altitude
780.584 km
Speed
7.464 km/s
True Right ascension
02h 25m 09s
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
09:51:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.267 km
Perigee altitude
773.004 km
Semi-major axis
7,152.772 km
Eccentricity
0.00023
Inclination
86.3991°
RAAN
36.288°
Arg. of periapsis
85.2886°
True anomaly
274.83095°
Mean anomaly
274.857°
Eccentric anomaly
274.84398°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00005572
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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 | 2026-05-22 03:41:10.911Z | 50.359° ENE | 2026-05-22 03:43:10.911Z | 73.737° E | 12.289° | 2026-05-22 03:45:10.911Z | 96.962° ESE |
| 8 mins | 2026-05-22 05:21:10.911Z | 349.355° N | 2026-05-22 05:24:10.911Z | 290.238° WNW | 43.229° | 2026-05-22 05:29:10.911Z | 187.628° SSW |
| 6 mins | 2026-05-22 16:37:10.911Z | 125.799° SE | 2026-05-22 16:40:10.911Z | 77.485° E | 24.055° | 2026-05-22 16:43:10.911Z | 34.558° NE |
| 7 mins | 2026-05-22 18:17:10.911Z | 224.945° SW | 2026-05-22 18:20:10.911Z | 272.464° WNW | 28.168° | 2026-05-22 18:24:10.911Z | 336.825° NNW |
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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