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, 4.8 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 114
1 41923U 17003G 25324.11974696 .00000077 00000-0 20367-4 0 9995
2 41923 86.4000 175.8054 0002022 81.7562 278.3863 14.34219227463289Epoch: 2025-11-20T02:52Z
TLE epoch observation values (Epoch: 2025-11-20T02:52:26.137Z)
Latitude
-0.00002°
Longitude
73.3148°
Altitude
780.502 km
Speed
7.464 km/s
True Right ascension
11h 43m 13s
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
10:07:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.073 km
Perigee altitude
773.18 km
Semi-major axis
7,152.764 km
Eccentricity
0.0002
Inclination
86.4°
RAAN
175.8054°
Arg. of periapsis
81.7562°
True anomaly
278.36338°
Mean anomaly
278.3863°
Eccentric anomaly
278.37484°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000020367
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-20 14:41:40.759Z | 174.583° S | 2025-11-20 14:46:40.759Z | 107.758° ESE | 43.929° | 2025-11-20 14:51:40.759Z | 6.362° NNE |
| 5 mins | 2025-11-21 01:14:40.759Z | 44.359° NE | 2025-11-21 01:16:40.759Z | 71.439° E | 17.99° | 2025-11-21 01:19:40.759Z | 112.287° ESE |
| 8 mins | 2025-11-21 02:54:40.759Z | 337.31° NNW | 2025-11-21 02:57:40.759Z | 283.484° WNW | 35.724° | 2025-11-21 03:02:40.759Z | 201.746° SSW |
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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