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 25298.51419796 .00000121 00000-0 36174-4 0 9993
2 42960 86.3940 123.3987 0002163 77.1639 282.9798 14.34214476421188Epoch: 2025-10-25T12:20Z
TLE epoch observation values (Epoch: 2025-10-25T12:20:26.703Z)
Latitude
-0.00008°
Longitude
-95.85622°
Altitude
780.382 km
Speed
7.464 km/s
True Right ascension
08h 13m 35s
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
17:21:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.19 km
Perigee altitude
773.095 km
Semi-major axis
7,152.78 km
Eccentricity
0.00022
Inclination
86.394°
RAAN
123.3987°
Arg. of periapsis
77.1639°
True anomaly
282.95565°
Mean anomaly
282.9798°
Eccentric anomaly
282.96772°
Mean motion
3.58782 °/min
Orbital period
100.34 mins
BSTAR
0.000036174
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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 | 2025-10-26 00:37:50.647Z | 357.405° N | 2025-10-26 00:42:50.647Z | 183.898° SSW | 44.943° | 2025-10-26 00:47:50.647Z | 179.239° S |
| 6 mins | 2025-10-26 11:55:50.647Z | 116.592° SE | 2025-10-26 11:57:50.647Z | 89.029° E | 19.637° | 2025-10-26 12:01:50.647Z | 35.756° NE |
| 7 mins | 2025-10-26 13:35:50.647Z | 219.619° SW | 2025-10-26 13:38:50.647Z | 280.959° WNW | 33.345° | 2025-10-26 13:42:50.647Z | 344.049° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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