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: 11 hours ago
TLE from 11 hours ago
0 IRIDIUM 114
1 41923U 17003G 26305.24136828 .00000039 00000-0 67395-5 0 9997
2 41923 86.4004 31.1419 0002046 95.9626 264.1803 14.34217980512899Epoch: 2026-11-01T05:47Z
TLE epoch observation values (Epoch: 2026-11-01T05:47:34.219Z)
Latitude
-0.00002°
Longitude
-96.28624°
Altitude
780.866 km
Speed
7.463 km/s
True Right ascension
02h 04m 34s
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
12:44:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.094 km
Perigee altitude
773.167 km
Semi-major axis
7,152.768 km
Eccentricity
0.0002
Inclination
86.4004°
RAAN
31.1419°
Arg. of periapsis
95.9626°
True anomaly
264.15698°
Mean anomaly
264.1803°
Eccentric anomaly
264.16864°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000067395
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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 | 2026-11-01 18:04:39.167Z | 356.679° N | 2026-11-01 18:09:39.167Z | 335.193° NNW | 81.753° | 2026-11-01 18:14:39.167Z | 180.547° SSW |
| 6 mins | 2026-11-02 05:22:39.167Z | 120.494° SE | 2026-11-02 05:25:39.167Z | 77.427° E | 22.062° | 2026-11-02 05:28:39.167Z | 37.709° NE |
| 8 mins | 2026-11-02 07:02:39.167Z | 218.493° SW | 2026-11-02 07:05:39.167Z | 272.212° WNW | 39.657° | 2026-11-02 07:10:39.167Z | 346.797° 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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