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: 8 hours ago
TLE from 8 hours ago
0 IRIDIUM 114
1 41923U 17003G 26035.37673664 .00000217 00000-0 70535-4 0 9992
2 41923 86.4025 143.9765 0002424 98.6177 261.5294 14.34219657474210Epoch: 2026-02-04T09:02Z
TLE epoch observation values (Epoch: 2026-02-04T09:02:30.045Z)
Latitude
0.00001°
Longitude
-126.19289°
Altitude
780.968 km
Speed
7.463 km/s
True Right ascension
09h 35m 54s
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
19:04:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.359 km
Perigee altitude
772.891 km
Semi-major axis
7,152.762 km
Eccentricity
0.00024
Inclination
86.4025°
RAAN
143.9765°
Arg. of periapsis
98.6177°
True anomaly
261.50193°
Mean anomaly
261.5294°
Eccentric anomaly
261.51566°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.000070535
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-04 18:00:56.418Z | 46.19° ENE | 2026-02-04 18:02:56.418Z | 71.123° E | 15.102° | 2026-02-04 18:05:56.418Z | 108.25° ESE |
| 8 mins | 2026-02-04 19:40:56.418Z | 343.282° N | 2026-02-04 19:43:56.418Z | 290.62° WNW | 39.471° | 2026-02-04 19:48:56.418Z | 195.427° SSW |
| 7 mins | 2026-02-05 06:56:56.418Z | 133.931° SE | 2026-02-05 06:59:56.418Z | 80.607° E | 28.357° | 2026-02-05 07:03:56.418Z | 24.555° NE |
| 6 mins | 2026-02-05 08:37:56.418Z | 239.415° WSW | 2026-02-05 08:40:56.418Z | 289.517° WNW | 23.847° | 2026-02-05 08:43:56.418Z | 331.142° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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