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: 6 hours ago
TLE from 6 hours ago
0 IRIDIUM 107
1 42960U 17061F 25319.72382819 .00000275 00000-0 91285-4 0 9999
2 42960 86.3943 114.5290 0001636 85.7878 274.3504 14.34221757424222Epoch: 2025-11-15T17:22Z
TLE epoch observation values (Epoch: 2025-11-15T17:22:18.755Z)
Latitude
-0.00011°
Longitude
158.90198°
Altitude
780.616 km
Speed
7.464 km/s
True Right ascension
07h 38m 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
20:12:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.789 km
Perigee altitude
773.448 km
Semi-major axis
7,152.755 km
Eccentricity
0.00016
Inclination
86.3943°
RAAN
114.529°
Arg. of periapsis
85.7878°
True anomaly
274.33171°
Mean anomaly
274.3504°
Eccentric anomaly
274.34105°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.000091285
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-16 10:14:19.128Z | 140.43° SSE | 2025-11-16 10:18:19.128Z | 81.425° E | 27.038° | 2025-11-16 10:22:19.128Z | 25.94° NE |
| 6 mins | 2025-11-16 11:56:19.128Z | 237.342° WSW | 2025-11-16 11:59:19.128Z | 289.453° WNW | 25.082° | 2025-11-16 12:02:19.128Z | 332.158° NNW |
| 9 mins | 2025-11-16 22:25:19.128Z | 3.863° NNE | 2025-11-16 22:29:19.128Z | 94.791° ESE | 43.602° | 2025-11-16 22:34:19.128Z | 171.46° 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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