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: 4 hours ago
TLE from 4 hours ago
0 IRIDIUM 114
1 41923U 17003G 25308.63113743 .00000157 00000-0 48876-4 0 9996
2 41923 86.4019 182.2684 0002195 80.4214 279.7230 14.34218030461069Epoch: 2025-11-04T15:08Z
TLE epoch observation values (Epoch: 2025-11-04T15:08:50.273Z)
Latitude
-0.00003°
Longitude
-89.05646°
Altitude
780.452 km
Speed
7.464 km/s
True Right ascension
12h 09m 04s
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
15:26:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.201 km
Perigee altitude
773.061 km
Semi-major axis
7,152.768 km
Eccentricity
0.00022
Inclination
86.4019°
RAAN
182.2684°
Arg. of periapsis
80.4214°
True anomaly
279.69821°
Mean anomaly
279.723°
Eccentric anomaly
279.7106°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000048876
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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 | 2025-11-05 03:26:06.348Z | 9.048° NNE | 2025-11-05 03:31:06.348Z | 87.073° E | 37.131° | 2025-11-05 03:35:06.348Z | 155.415° SSE |
| 5 mins | 2025-11-05 05:09:06.348Z | 309.652° NW | 2025-11-05 05:11:06.348Z | 283.073° WNW | 17.052° | 2025-11-05 05:14:06.348Z | 244.405° WSW |
| 9 mins | 2025-11-05 16:23:06.348Z | 188.312° SSW | 2025-11-05 16:27:06.348Z | 289.19° WNW | 44.133° | 2025-11-05 16:32:06.348Z | 359.302° 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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