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 25363.81753216 -.00000010 00000-0 -10562-4 0 9999
2 42960 86.3969 96.0989 0002319 105.4416 254.7036 14.34217314430544Epoch: 2025-12-29T19:37Z
TLE epoch observation values (Epoch: 2025-12-29T19:37:14.778Z)
Latitude
-0.00004°
Longitude
63.27761°
Altitude
781.158 km
Speed
7.463 km/s
True Right ascension
06h 24m 23s
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
01:31:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.292 km
Perigee altitude
772.974 km
Semi-major axis
7,152.77 km
Eccentricity
0.00023
Inclination
86.3969°
RAAN
96.0989°
Arg. of periapsis
105.4416°
True anomaly
254.67797°
Mean anomaly
254.7036°
Eccentric anomaly
254.69078°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000010562
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-30 05:47:52.807Z | 124.733° SE | 2025-12-30 05:51:52.807Z | 73.512° E | 18.475° | 2025-12-30 05:54:52.807Z | 37.092° NE |
| 8 mins | 2025-12-30 07:27:52.807Z | 209.266° SW | 2025-12-30 07:31:52.807Z | 280.495° WNW | 34.981° | 2025-12-30 07:35:52.807Z | 345.531° N |
| 8 mins | 2025-12-30 17:58:52.807Z | 19.065° NNE | 2025-12-30 18:01:52.807Z | 71.993° E | 34.88° | 2025-12-30 18:06:52.807Z | 154.785° SSE |
| 5 mins | 2025-12-30 19:40:52.807Z | 303.923° NW | 2025-12-30 19:42:52.807Z | 274.406° WNW | 18.413° | 2025-12-30 19:45:52.807Z | 237.293° WSW |
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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