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: 13 hours ago
TLE from 13 hours ago
0 IRIDIUM 107
1 42960U 17061F 25258.74614536 .00000186 00000-0 59186-4 0 9992
2 42960 86.4000 140.0178 0002463 92.2503 267.8975 14.34220427415483Epoch: 2025-09-15T17:54Z
TLE epoch observation values (Epoch: 2025-09-15T17:54:26.959Z)
Latitude
0.00001°
Longitude
-123.54091°
Altitude
780.774 km
Speed
7.463 km/s
True Right ascension
09h 20m 04s
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
23:10:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.384 km
Perigee altitude
772.861 km
Semi-major axis
7,152.76 km
Eccentricity
0.00025
Inclination
86.4°
RAAN
140.0178°
Arg. of periapsis
92.2503°
True anomaly
267.8693°
Mean anomaly
267.8975°
Eccentric anomaly
267.8834°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.000059186
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Other satellites on launch #61 in the year 2017 (2017-10-09 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-16 15:48:16.202Z | 132.544° SE | 2025-09-16 15:52:16.202Z | 73.546° E | 23.473° | 2025-09-16 15:55:16.202Z | 33.136° NE |
| 7 mins | 2025-09-16 17:29:16.202Z | 226.213° WSW | 2025-09-16 17:32:16.202Z | 277.414° WNW | 28.724° | 2025-09-16 17:36:16.202Z | 338.766° N |
| 8 mins | 2025-09-17 03:59:16.202Z | 10.128° NNE | 2025-09-17 04:02:16.202Z | 59.078° ENE | 40.263° | 2025-09-17 04:07:16.202Z | 164.436° S |
| 4 mins | 2025-09-17 05:41:16.202Z | 302.011° NW | 2025-09-17 05:43:16.202Z | 276.62° WNW | 14.03° | 2025-09-17 05:45:16.202Z | 252.95° W |
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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