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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 107
1 42960U 17061F 25312.74698736 .00000169 00000-0 53394-4 0 9993
2 42960 86.3941 117.4466 0001779 80.2828 279.8568 14.34218428423220Epoch: 2025-11-08T17:55Z
TLE epoch observation values (Epoch: 2025-11-08T17:55:39.707Z)
Latitude
-0.00012°
Longitude
160.35898°
Altitude
780.498 km
Speed
7.464 km/s
True Right ascension
07h 49m 47s
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
22:40:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.902 km
Perigee altitude
773.357 km
Semi-major axis
7,152.766 km
Eccentricity
0.00018
Inclination
86.3941°
RAAN
117.4466°
Arg. of periapsis
80.2828°
True anomaly
279.83671°
Mean anomaly
279.8568°
Eccentric anomaly
279.84676°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000053394
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-09 10:47:50.676Z | 135.506° SSE | 2025-11-09 10:51:50.676Z | 77.995° E | 24.441° | 2025-11-09 10:55:50.676Z | 26.999° NE |
| 7 mins | 2025-11-09 12:28:50.676Z | 225.296° WSW | 2025-11-09 12:31:50.676Z | 271.906° WNW | 27.744° | 2025-11-09 12:35:50.676Z | 336.206° NNW |
| 8 mins | 2025-11-09 22:58:50.676Z | 7.936° NNE | 2025-11-09 23:02:50.676Z | 103.306° ESE | 41.514° | 2025-11-09 23:06:50.676Z | 165.241° S |
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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