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: 4 hours ago
TLE from 4 hours ago
0 IRIDIUM 132
1 42961U 17061G 25322.45114222 .00000241 00000-0 78964-4 0 9997
2 42961 86.3948 113.3696 0001903 92.1371 268.0042 14.34217535424611Epoch: 2025-11-18T10:49Z
TLE epoch observation values (Epoch: 2025-11-18T10:49:38.687Z)
Latitude
-0.00012°
Longitude
-106.77864°
Altitude
780.766 km
Speed
7.463 km/s
True Right ascension
07h 33m 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
12:03:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.994 km
Perigee altitude
773.271 km
Semi-major axis
7,152.769 km
Eccentricity
0.00019
Inclination
86.3948°
RAAN
113.3696°
Arg. of periapsis
92.1371°
True anomaly
267.98241°
Mean anomaly
268.0042°
Eccentric anomaly
267.9933°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000078964
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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 | 2025-11-18 21:27:17.221Z | 26.179° NE | 2025-11-18 21:31:17.221Z | 82.008° E | 23.457° | 2025-11-18 21:35:17.221Z | 134.059° SE |
| 8 mins | 2025-11-18 23:08:17.221Z | 332.135° NNW | 2025-11-18 23:12:17.221Z | 265.017° W | 28.762° | 2025-11-18 23:16:17.221Z | 213.18° SW |
| 9 mins | 2025-11-19 10:23:17.221Z | 161.376° S | 2025-11-19 10:27:17.221Z | 89.301° E | 39.304° | 2025-11-19 10:32:17.221Z | 11.958° NNE |
| 5 mins | 2025-11-19 12:06:17.221Z | 257.578° W | 2025-11-19 12:08:17.221Z | 283.391° WNW | 15.653° | 2025-11-19 12:11:17.221Z | 320.379° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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