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: 11 hours ago
TLE from 11 hours ago
0 IRIDIUM 107
1 42960U 17061F 26275.93808745 -.00000001 00000-0 -75177-5 0 9997
2 42960 86.4006 340.2537 0001946 91.0519 269.0899 14.34217343470260Epoch: 2026-10-02T22:30Z
TLE epoch observation values (Epoch: 2026-10-02T22:30:50.755Z)
Latitude
-0.00011°
Longitude
-9.11065°
Altitude
780.742 km
Speed
7.463 km/s
True Right ascension
22h 41m 00s
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
03:28:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.025 km
Perigee altitude
773.241 km
Semi-major axis
7,152.77 km
Eccentricity
0.00019
Inclination
86.4006°
RAAN
340.2537°
Arg. of periapsis
91.0519°
True anomaly
269.0676°
Mean anomaly
269.0899°
Eccentric anomaly
269.07875°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000075177
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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 | 2026-10-03 15:49:51.444Z | 17.642° NNE | 2026-10-03 15:53:51.444Z | 69.558° E | 33.177° | 2026-10-03 15:58:51.444Z | 144.754° SSE |
| 7 mins | 2026-10-03 17:31:51.444Z | 322.545° NNW | 2026-10-03 17:34:51.444Z | 277.749° WNW | 25.931° | 2026-10-03 17:38:51.444Z | 224.392° SW |
| 8 mins | 2026-10-04 04:46:51.444Z | 171.463° S | 2026-10-04 04:49:51.444Z | 134.073° SE | 67.908° | 2026-10-04 04:54:51.444Z | 7.128° NNE |
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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