IRIDIUM 107, 42960
Orbit data source: Space-Track
IRIDIUM 107, 42960 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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42960 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 107
1 42960U 17061F 25333.81706714 .00000036 00000-0 56308-5 0 9992
2 42960 86.3955 108.6367 0001669 102.2857 257.8525 14.34217830426242Epoch: 2025-11-29T19:36Z
TLE epoch observation values (Epoch: 2025-11-29T19:36:34.600Z)
Latitude
-0.00012°
Longitude
105.55269°
Altitude
780.969 km
Speed
7.463 km/s
True Right ascension
07h 14m 32s
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
21:17:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.825 km
Perigee altitude
773.438 km
Semi-major axis
7,152.768 km
Eccentricity
0.00017
Inclination
86.3955°
RAAN
108.6367°
Arg. of periapsis
102.2857°
True anomaly
257.8338°
Mean anomaly
257.8525°
Eccentric anomaly
257.84315°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000056308
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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 107 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-30 09:07:04.610Z | 151.765° SSE | 2025-11-30 09:11:04.610Z | 97.554° ESE | 32.12° | 2025-11-30 09:16:04.610Z | 19.02° NNE |
| 6 mins | 2025-11-30 10:50:04.610Z | 248.337° W | 2025-11-30 10:52:04.610Z | 277.979° WNW | 20.618° | 2025-11-30 10:56:04.610Z | 331.023° NNW |
| 8 mins | 2025-11-30 21:19:04.610Z | 356.768° N | 2025-11-30 21:23:04.610Z | 187.847° SSW | 43.945° | 2025-11-30 21:27:04.610Z | 180.199° SSW |
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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