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: 5 hours ago
TLE from 5 hours ago
0 IRIDIUM 107
1 42960U 17061F 26038.16697586 .00000195 00000-0 62415-4 0 9990
2 42960 86.3922 79.6419 0002308 83.2497 276.8962 14.34218136436180Epoch: 2026-02-07T04:00Z
TLE epoch observation values (Epoch: 2026-02-07T04:00:26.714Z)
Latitude
0.00005°
Longitude
-117.7638°
Altitude
780.519 km
Speed
7.464 km/s
True Right ascension
05h 18m 34s
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
10:55:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.281 km
Perigee altitude
772.98 km
Semi-major axis
7,152.767 km
Eccentricity
0.00023
Inclination
86.3922°
RAAN
79.6419°
Arg. of periapsis
83.2497°
True anomaly
276.86994°
Mean anomaly
276.8962°
Eccentric anomaly
276.88307°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000062415
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-02-07 14:37:12.200Z | 3.02° NNE | 2026-02-07 14:42:12.200Z | 83.906° E | 42.832° | 2026-02-07 14:47:12.200Z | 169.226° S |
| 4 mins | 2026-02-08 01:56:12.200Z | 102.058° ESE | 2026-02-08 01:58:12.200Z | 75.919° E | 15.281° | 2026-02-08 02:00:12.200Z | 50.836° ENE |
| 9 mins | 2026-02-08 03:34:12.200Z | 200.575° SSW | 2026-02-08 03:38:12.200Z | 276.424° WNW | 39.54° | 2026-02-08 03:43:12.200Z | 353.411° N |
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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