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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 IRIDIUM 132
1 42961U 17061G 25258.75248545 -.00000017 00000-0 -13039-4 0 9999
2 42961 86.4001 139.9967 0002253 86.8374 273.3079 14.34217707415484Epoch: 2025-09-15T18:03Z
TLE epoch observation values (Epoch: 2025-09-15T18:03:34.742Z)
Latitude
-0.0001°
Longitude
-125.85069°
Altitude
780.626 km
Speed
7.464 km/s
True Right ascension
09h 19m 59s
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
23:10:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.243 km
Perigee altitude
773.02 km
Semi-major axis
7,152.769 km
Eccentricity
0.00023
Inclination
86.4001°
RAAN
139.9967°
Arg. of periapsis
86.8374°
True anomaly
273.28213°
Mean anomaly
273.3079°
Eccentric anomaly
273.29501°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000013039
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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 | 2025-09-16 15:57:16.300Z | 139.458° SSE | 2025-09-16 16:01:16.300Z | 74.952° E | 27.5° | 2025-09-16 16:05:16.300Z | 23.634° NE |
| 7 mins | 2025-09-16 17:38:16.300Z | 230.973° WSW | 2025-09-16 17:41:16.300Z | 274.914° WNW | 24.572° | 2025-09-16 17:45:16.300Z | 333.799° NNW |
| 8 mins | 2025-09-17 04:08:16.300Z | 3.518° NNE | 2025-09-17 04:12:16.300Z | 124.53° SE | 43.442° | 2025-09-17 04:16:16.300Z | 171.652° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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