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: 6 hours ago
TLE from 6 hours ago
0 IRIDIUM 107
1 42960U 17061F 25342.81720740 .00000531 00000-0 18260-3 0 9990
2 42960 86.3964 104.8752 0001831 106.8855 253.2542 14.34218224427537Epoch: 2025-12-08T19:36Z
TLE epoch observation values (Epoch: 2025-12-08T19:36:46.719Z)
Latitude
0.00002°
Longitude
92.86974°
Altitude
781.094 km
Speed
7.463 km/s
True Right ascension
06h 59m 30s
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
23:29:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.94 km
Perigee altitude
773.32 km
Semi-major axis
7,152.767 km
Eccentricity
0.00018
Inclination
86.3964°
RAAN
104.8752°
Arg. of periapsis
106.8855°
True anomaly
253.23411°
Mean anomaly
253.2542°
Eccentric anomaly
253.24415°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0001826
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-09 07:29:56.659Z | 97.661° ESE | 2025-12-09 07:31:56.659Z | 73.382° E | 12.909° | 2025-12-09 07:33:56.659Z | 50.386° ENE |
| 8 mins | 2025-12-09 09:07:56.659Z | 194.538° SSW | 2025-12-09 09:11:56.659Z | 293.227° NW | 42.229° | 2025-12-09 09:15:56.659Z | 354.853° N |
| 7 mins | 2025-12-09 19:38:56.659Z | 29.256° NE | 2025-12-09 19:41:56.659Z | 77.444° E | 26.968° | 2025-12-09 19:45:56.659Z | 137.528° SSE |
| 7 mins | 2025-12-09 21:19:56.659Z | 321.332° NNW | 2025-12-09 21:22:56.659Z | 271.272° WNW | 25.297° | 2025-12-09 21:26:56.659Z | 219.634° SW |
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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