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: 15 hours ago
TLE from 15 hours ago
0 IRIDIUM 114
1 41923U 17003G 25353.98066586 .00000057 00000-0 13184-4 0 9999
2 41923 86.3990 163.3387 0001832 93.8528 266.2877 14.34217098467561Epoch: 2025-12-19T23:32Z
TLE epoch observation values (Epoch: 2025-12-19T23:32:09.530Z)
Latitude
-0.00004°
Longitude
81.48496°
Altitude
780.805 km
Speed
7.463 km/s
True Right ascension
10h 53m 21s
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
13:36:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.944 km
Perigee altitude
773.323 km
Semi-major axis
7,152.771 km
Eccentricity
0.00018
Inclination
86.399°
RAAN
163.3387°
Arg. of periapsis
93.8528°
True anomaly
266.26675°
Mean anomaly
266.2877°
Eccentric anomaly
266.27723°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000013184
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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 | 2025-12-20 23:33:14.000Z | 359.193° N | 2025-12-20 23:37:14.000Z | 17.442° NNE | 43.829° | 2025-12-20 23:42:14.000Z | 176.418° S |
| 5 mins | 2025-12-21 10:51:14.000Z | 110.45° ESE | 2025-12-21 10:53:14.000Z | 82.205° E | 18.659° | 2025-12-21 10:56:14.000Z | 42.129° NE |
| 8 mins | 2025-12-21 12:30:14.000Z | 212.053° SW | 2025-12-21 12:33:14.000Z | 261.846° W | 34.467° | 2025-12-21 12:38:14.000Z | 347.637° 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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