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: 10 hours ago
TLE from 10 hours ago
0 IRIDIUM 107
1 42960U 17061F 25289.58382818 .00000128 00000-0 38562-4 0 9994
2 42960 86.3945 127.1329 0002384 77.8963 282.2500 14.34218354419907Epoch: 2025-10-16T14:00Z
TLE epoch observation values (Epoch: 2025-10-16T14:00:42.754Z)
Latitude
-0.00002°
Longitude
-108.3867°
Altitude
780.354 km
Speed
7.464 km/s
True Right ascension
08h 28m 31s
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
18:44:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.335 km
Perigee altitude
772.924 km
Semi-major axis
7,152.767 km
Eccentricity
0.00024
Inclination
86.3945°
RAAN
127.1329°
Arg. of periapsis
77.8963°
True anomaly
282.2233°
Mean anomaly
282.25°
Eccentric anomaly
282.23665°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000038562
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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 | 2025-10-17 00:38:19.650Z | 23.397° NE | 2025-10-17 00:42:19.650Z | 81.599° E | 26.189° | 2025-10-17 00:46:19.650Z | 137.689° SSE |
| 6 mins | 2025-10-17 02:20:19.650Z | 320.129° NNW | 2025-10-17 02:23:19.650Z | 267.091° W | 25.908° | 2025-10-17 02:26:19.650Z | 224.266° SW |
| 9 mins | 2025-10-17 13:34:19.650Z | 166.946° S | 2025-10-17 13:38:19.650Z | 91.945° ESE | 41.886° | 2025-10-17 13:43:19.650Z | 9.35° 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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