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: 13 hours ago
TLE from 13 hours ago
0 IRIDIUM 114
1 41923U 17003G 26100.05215523 -.00000003 00000-0 -83109-5 0 9993
2 41923 86.3931 116.9580 0001988 94.8064 265.3359 14.34217504483489Epoch: 2026-04-10T01:15Z
TLE epoch observation values (Epoch: 2026-04-10T01:15:06.211Z)
Latitude
-0.00003°
Longitude
-100.10924°
Altitude
780.835 km
Speed
7.463 km/s
True Right ascension
07h 47m 49s
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
20:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.055 km
Perigee altitude
773.211 km
Semi-major axis
7,152.77 km
Eccentricity
0.0002
Inclination
86.3931°
RAAN
116.958°
Arg. of periapsis
94.8064°
True anomaly
265.3132°
Mean anomaly
265.3359°
Eccentric anomaly
265.32455°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000083109
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-11 00:48:52.377Z | 140.813° SSE | 2026-04-11 00:52:52.377Z | 83.779° E | 26.825° | 2026-04-11 00:56:52.377Z | 26.832° NE |
| 7 mins | 2026-04-11 02:30:52.377Z | 235.814° WSW | 2026-04-11 02:33:52.377Z | 287.373° WNW | 25.414° | 2026-04-11 02:37:52.377Z | 338.991° N |
| 9 mins | 2026-04-11 12:59:52.377Z | 3.922° NNE | 2026-04-11 13:03:52.377Z | 83.864° E | 43.489° | 2026-04-11 13:08:52.377Z | 170.925° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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