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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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: 5 hours ago
TLE from 5 hours ago
0 IRIDIUM 107
1 42960U 17061F 26128.16836515 .00000007 00000-0 -45445-5 0 9995
2 42960 86.3992 41.9944 0002375 83.1140 277.0326 14.34217646449085Epoch: 2026-05-08T04:02Z
TLE epoch observation values (Epoch: 2026-05-08T04:02:26.748Z)
Latitude
-0.00005°
Longitude
115.37892°
Altitude
780.511 km
Speed
7.464 km/s
True Right ascension
02h 47m 58s
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
16:45:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.331 km
Perigee altitude
772.933 km
Semi-major axis
7,152.769 km
Eccentricity
0.00024
Inclination
86.3992°
RAAN
41.9944°
Arg. of periapsis
83.114°
True anomaly
277.00559°
Mean anomaly
277.0326°
Eccentric anomaly
277.01909°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000045445
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-08 17:34:45.418Z | 115.062° SE | 2026-05-08 17:37:45.418Z | 77.495° E | 16.329° | 2026-05-08 17:40:45.418Z | 41.244° NE |
| 8 mins | 2026-05-08 19:14:45.418Z | 208.176° SW | 2026-05-08 19:17:45.418Z | 271.169° WNW | 38.105° | 2026-05-08 19:22:45.418Z | 351.735° N |
| 8 mins | 2026-05-09 05:44:45.418Z | 21.041° NNE | 2026-05-09 05:48:45.418Z | 95.027° ESE | 31.525° | 2026-05-09 05:52:45.418Z | 148.938° SSE |
| 5 mins | 2026-05-09 07:26:45.418Z | 309.117° NW | 2026-05-09 07:28:45.418Z | 278.065° WNW | 21.004° | 2026-05-09 07:31:45.418Z | 236.223° 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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