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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 132
1 42961U 17061G 25307.72998347 .00000001 00000-0 -68101-5 0 9996
2 42961 86.3938 119.5254 0001914 87.6023 272.5392 14.34217349422500Epoch: 2025-11-03T17:31Z
TLE epoch observation values (Epoch: 2025-11-03T17:31:10.571Z)
Latitude
-0.00003°
Longitude
173.50418°
Altitude
780.659 km
Speed
7.464 km/s
True Right ascension
07h 58m 06s
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
22:38:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.002 km
Perigee altitude
773.264 km
Semi-major axis
7,152.77 km
Eccentricity
0.00019
Inclination
86.3938°
RAAN
119.5254°
Arg. of periapsis
87.6023°
True anomaly
272.51729°
Mean anomaly
272.5392°
Eccentric anomaly
272.52824°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000068101
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-04 12:02:21.988Z | 176.491° S | 2025-11-04 12:07:21.988Z | 102.765° ESE | 44.507° | 2025-11-04 12:12:21.988Z | 5.134° NNE |
| 6 mins | 2025-11-04 22:35:21.988Z | 44.345° NE | 2025-11-04 22:37:21.988Z | 72.387° E | 18.957° | 2025-11-04 22:41:21.988Z | 123.506° SE |
| 8 mins | 2025-11-05 00:15:21.988Z | 335.146° NNW | 2025-11-05 00:18:21.988Z | 280.282° WNW | 34.555° | 2025-11-05 00:23:21.988Z | 203.354° SW |
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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