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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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: 6 hours ago
TLE from 6 hours ago
0 IRIDIUM 132
1 42961U 17061G 25291.96229916 .00000012 00000-0 -27977-5 0 9991
2 42961 86.3946 126.1194 0001996 83.6766 276.4657 14.34217988420241Epoch: 2025-10-18T23:05Z
TLE epoch observation values (Epoch: 2025-10-18T23:05:42.647Z)
Latitude
-0.00003°
Longitude
112.00591°
Altitude
780.557 km
Speed
7.464 km/s
True Right ascension
08h 24m 28s
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
00:23:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.059 km
Perigee altitude
773.203 km
Semi-major axis
7,152.768 km
Eccentricity
0.0002
Inclination
86.3946°
RAAN
126.1194°
Arg. of periapsis
83.6766°
True anomaly
276.44297°
Mean anomaly
276.4657°
Eccentric anomaly
276.45434°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000027977
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-19 12:36:49.551Z | 131.734° SE | 2025-10-19 12:40:49.551Z | 80.639° E | 21.168° | 2025-10-19 12:43:49.551Z | 38.847° NE |
| 8 mins | 2025-10-19 14:17:49.551Z | 218.224° SW | 2025-10-19 14:20:49.551Z | 267.146° W | 31.443° | 2025-10-19 14:25:49.551Z | 345.268° N |
| 8 mins | 2025-10-20 00:47:49.551Z | 12.32° NNE | 2025-10-20 00:51:49.551Z | 92.12° ESE | 38.265° | 2025-10-20 00:55:49.551Z | 158.01° S |
| 5 mins | 2025-10-20 02:29:49.551Z | 307.708° NW | 2025-10-20 02:31:49.551Z | 281.449° WNW | 16.194° | 2025-10-20 02:34:49.551Z | 244.434° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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