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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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: 7 hours ago
TLE from 7 hours ago
0 IRIDIUM 114
1 41923U 17003G 26319.47414633 .00000002 00000-0 -63218-5 0 9991
2 41923 86.3993 25.1968 0001990 97.9738 262.1684 14.34217515514936Epoch: 2026-11-15T11:22Z
TLE epoch observation values (Epoch: 2026-11-15T11:22:46.242Z)
Latitude
-0.00002°
Longitude
159.94006°
Altitude
780.913 km
Speed
7.463 km/s
True Right ascension
01h 40m 47s
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
14:37:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.056 km
Perigee altitude
773.209 km
Semi-major axis
7,152.769 km
Eccentricity
0.0002
Inclination
86.3993°
RAAN
25.1968°
Arg. of periapsis
97.9738°
True anomaly
262.14581°
Mean anomaly
262.1684°
Eccentric anomaly
262.1571°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000063218
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-16 04:15:05.338Z | 135.316° SSE | 2026-11-16 04:19:05.338Z | 74.73° E | 27.94° | 2026-11-16 04:22:05.338Z | 32.458° NE |
| 7 mins | 2026-11-16 05:56:05.338Z | 227.854° WSW | 2026-11-16 05:59:05.338Z | 275.578° WNW | 30.916° | 2026-11-16 06:03:05.338Z | 336.56° NNW |
| 8 mins | 2026-11-16 16:26:05.338Z | 7.316° NNE | 2026-11-16 16:30:05.338Z | 111.983° ESE | 63.54° | 2026-11-16 16:34:05.338Z | 166.888° S |
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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