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: 13 hours ago
TLE from 13 hours ago
0 IRIDIUM 132
1 42961U 17061G 25356.56794783 .00000259 00000-0 85423-4 0 9999
2 42961 86.3970 99.1092 0002118 100.3991 259.7444 14.34218863429507Epoch: 2025-12-22T13:37Z
TLE epoch observation values (Epoch: 2025-12-22T13:37:50.692Z)
Latitude
0.00001°
Longitude
163.2838°
Altitude
780.985 km
Speed
7.463 km/s
True Right ascension
06h 36m 26s
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
01:16:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.143 km
Perigee altitude
773.113 km
Semi-major axis
7,152.765 km
Eccentricity
0.00021
Inclination
86.397°
RAAN
99.1092°
Arg. of periapsis
100.3991°
True anomaly
259.72052°
Mean anomaly
259.7444°
Eccentric anomaly
259.73246°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000085423
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-23 06:30:59.844Z | 120.53° SE | 2025-12-23 06:33:59.844Z | 78.883° E | 19.878° | 2025-12-23 06:36:59.844Z | 39.042° NE |
| 8 mins | 2025-12-23 08:10:59.844Z | 216.378° SW | 2025-12-23 08:13:59.844Z | 269.413° W | 33.223° | 2025-12-23 08:18:59.844Z | 347.156° N |
| 8 mins | 2025-12-23 18:40:59.844Z | 14.825° NNE | 2025-12-23 18:44:59.844Z | 95.293° ESE | 36.528° | 2025-12-23 18:48:59.844Z | 155.806° SSE |
| 5 mins | 2025-12-23 20:22:59.844Z | 307.337° NW | 2025-12-23 20:24:59.844Z | 279.853° WNW | 17.331° | 2025-12-23 20:27:59.844Z | 241.987° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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