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 26275.94442960 .00000004 00000-0 -56056-5 0 9999
2 42961 86.4006 340.2299 0002097 94.7605 265.3830 14.34217637470260Epoch: 2026-10-02T22:39Z
TLE epoch observation values (Epoch: 2026-10-02T22:39:58.717Z)
Latitude
-0.00005°
Longitude
-11.42387°
Altitude
780.84 km
Speed
7.463 km/s
True Right ascension
22h 40m 55s
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
03:28:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.132 km
Perigee altitude
773.132 km
Semi-major axis
7,152.769 km
Eccentricity
0.00021
Inclination
86.4006°
RAAN
340.2299°
Arg. of periapsis
94.7605°
True anomaly
265.35905°
Mean anomaly
265.383°
Eccentric anomaly
265.37102°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000056056
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-03 15:59:28.757Z | 16.332° NNE | 2026-10-03 16:03:28.757Z | 80.712° E | 41.295° | 2026-10-03 16:07:28.757Z | 148.221° SSE |
| 6 mins | 2026-10-03 17:41:28.757Z | 314.11° NW | 2026-10-03 17:43:28.757Z | 286.371° WNW | 21.105° | 2026-10-03 17:47:28.757Z | 233.382° WSW |
| 9 mins | 2026-10-04 04:55:28.757Z | 180.863° SSW | 2026-10-04 04:59:28.757Z | 127.855° SE | 89.609° | 2026-10-04 05:04:28.757Z | 2.586° NNE |
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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