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: 12 hours ago
TLE from 12 hours ago
0 IRIDIUM 107
1 42960U 17061F 26095.93532119 .00000395 00000-0 13390-3 0 9997
2 42960 86.3961 55.4634 0002222 94.6352 265.5097 14.34215628444462Epoch: 2026-04-05T22:26Z
TLE epoch observation values (Epoch: 2026-04-05T22:26:51.750Z)
Latitude
-0.00011°
Longitude
-115.48584°
Altitude
780.85 km
Speed
7.463 km/s
True Right ascension
03h 41m 51s
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
16:20:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.228 km
Perigee altitude
773.049 km
Semi-major axis
7,152.776 km
Eccentricity
0.00022
Inclination
86.3961°
RAAN
55.4634°
Arg. of periapsis
94.6352°
True anomaly
265.48432°
Mean anomaly
265.5097°
Eccentric anomaly
265.49701°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0001339
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-06 10:46:06.793Z | 314.184° NW | 2026-04-06 10:49:06.793Z | 276.874° WNW | 15.39° | 2026-04-06 10:51:06.793Z | 251.96° W |
| 8 mins | 2026-04-06 22:01:06.793Z | 194.087° SSW | 2026-04-06 22:04:06.793Z | 240.141° WSW | 42.144° | 2026-04-06 22:09:06.793Z | 356.24° N |
| 7 mins | 2026-04-07 08:32:06.793Z | 32.789° NE | 2026-04-07 08:35:06.793Z | 83.706° E | 26.329° | 2026-04-07 08:39:06.793Z | 138.607° SSE |
| 6 mins | 2026-04-07 10:13:06.793Z | 318.822° NNW | 2026-04-07 10:15:06.793Z | 286.12° WNW | 25.707° | 2026-04-07 10:19:06.793Z | 223.747° 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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