IRIDIUM 114, 41923
Orbit data source: Space-Track
IRIDIUM 114, 41923 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 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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41923 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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 IRIDIUM 114
1 41923U 17003G 25256.93266419 .00000246 00000-0 80960-4 0 9999
2 41923 86.4023 203.8320 0002276 86.7360 273.4096 14.34216366453659Epoch: 2025-09-13T22:23Z
TLE epoch observation values (Epoch: 2025-09-13T22:23:02.186Z)
Latitude
-0.00001°
Longitude
-125.08603°
Altitude
780.626 km
Speed
7.464 km/s
True Right ascension
13h 35m 19s
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
22:25:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.264 km
Perigee altitude
773.008 km
Semi-major axis
7,152.773 km
Eccentricity
0.00023
Inclination
86.4023°
RAAN
203.832°
Arg. of periapsis
86.736°
True anomaly
273.38356°
Mean anomaly
273.4096°
Eccentric anomaly
273.39658°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00008096
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Other satellites on launch #3 in the year 2017 (2017-01-14 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 114 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 | 2025-09-14 07:21:17.108Z | 45.326° ENE | 2025-09-14 07:23:17.108Z | 68.915° E | 13.709° | 2025-09-14 07:26:17.108Z | 104.891° ESE |
| 8 mins | 2025-09-14 09:01:17.108Z | 346.946° N | 2025-09-14 09:05:17.108Z | 245.071° WSW | 41.046° | 2025-09-14 09:09:17.108Z | 192.448° SSW |
| 7 mins | 2025-09-14 20:17:17.108Z | 132.741° SE | 2025-09-14 20:20:17.108Z | 84.91° E | 26.404° | 2025-09-14 20:24:17.108Z | 27.545° NE |
| 7 mins | 2025-09-14 21:58:17.108Z | 234.644° WSW | 2025-09-14 22:01:17.108Z | 286.404° WNW | 25.843° | 2025-09-14 22:05:17.108Z | 338.995° N |
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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