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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 IRIDIUM 107
1 42960U 17061F 25259.58336610 .00000180 00000-0 57165-4 0 9998
2 42960 86.3998 139.6683 0002456 91.7548 268.3929 14.34220614415605Epoch: 2025-09-16T14:00Z
TLE epoch observation values (Epoch: 2025-09-16T14:00:02.831Z)
Latitude
-0.00001°
Longitude
-66.11508°
Altitude
780.758 km
Speed
7.463 km/s
True Right ascension
09h 18m 40s
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
22:06:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.379 km
Perigee altitude
772.865 km
Semi-major axis
7,152.759 km
Eccentricity
0.00025
Inclination
86.3998°
RAAN
139.6683°
Arg. of periapsis
91.7548°
True anomaly
268.36477°
Mean anomaly
268.3929°
Eccentric anomaly
268.37883°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.000057165
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-17 05:40:24.047Z | 311.441° NW | 2025-09-17 05:42:24.047Z | 288° WNW | 13.987° | 2025-09-17 05:45:24.047Z | 251.64° W |
| 8 mins | 2025-09-17 16:55:24.047Z | 199.022° SSW | 2025-09-17 16:58:24.047Z | 256.652° W | 41.196° | 2025-09-17 17:03:24.047Z | 354.627° N |
| 7 mins | 2025-09-18 03:26:24.047Z | 32.52° NE | 2025-09-18 03:29:24.047Z | 87.989° E | 28.083° | 2025-09-18 03:33:24.047Z | 142.387° SSE |
| 7 mins | 2025-09-18 05:06:24.047Z | 325.321° NNW | 2025-09-18 05:09:24.047Z | 282.124° WNW | 24.134° | 2025-09-18 05:13:24.047Z | 224.999° SW |
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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