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: 14 hours ago
TLE from 14 hours ago
0 IRIDIUM 114
1 41923U 17003G 25261.25831291 .00000092 00000-0 25878-4 0 9992
2 41923 86.4025 202.0265 0002346 89.0503 271.0961 14.34217755454270Epoch: 2025-09-18T06:11Z
TLE epoch observation values (Epoch: 2025-09-18T06:11:58.235Z)
Latitude
-0.00008°
Longitude
111.61136°
Altitude
780.686 km
Speed
7.464 km/s
True Right ascension
13h 28m 06s
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
13:31:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.31 km
Perigee altitude
772.953 km
Semi-major axis
7,152.769 km
Eccentricity
0.00023
Inclination
86.4025°
RAAN
202.0265°
Arg. of periapsis
89.0503°
True anomaly
271.06922°
Mean anomaly
271.0961°
Eccentric anomaly
271.08266°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000025878
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-18 21:23:10.687Z | 213.362° SW | 2025-09-18 21:27:10.687Z | 269.931° W | 30.81° | 2025-09-18 21:32:10.687Z | 345.068° N |
| 8 mins | 2025-09-19 07:54:10.687Z | 11.885° NNE | 2025-09-19 07:58:10.687Z | 96.787° ESE | 38.824° | 2025-09-19 08:02:10.687Z | 159.626° S |
| 5 mins | 2025-09-19 09:36:10.687Z | 306.283° NW | 2025-09-19 09:38:10.687Z | 280.167° WNW | 15.682° | 2025-09-19 09:41:10.687Z | 244.206° WSW |
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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