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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 114
1 41923U 17003G 25310.16604332 .00000282 00000-0 93714-4 0 9996
2 41923 86.4017 181.6280 0002163 80.3211 279.8229 14.34219361461284Epoch: 2025-11-06T03:59Z
TLE epoch observation values (Epoch: 2025-11-06T03:59:06.142Z)
Latitude
-0.00005°
Longitude
76.22414°
Altitude
780.449 km
Speed
7.464 km/s
True Right ascension
12h 06m 30s
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
09:17:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.173 km
Perigee altitude
773.079 km
Semi-major axis
7,152.763 km
Eccentricity
0.00022
Inclination
86.4017°
RAAN
181.628°
Arg. of periapsis
80.3211°
True anomaly
279.79848°
Mean anomaly
279.8229°
Eccentric anomaly
279.81069°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000093714
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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 | 2025-11-06 15:49:12.091Z | 163.964° S | 2025-11-06 15:53:12.091Z | 103.703° ESE | 39.843° | 2025-11-06 15:58:12.091Z | 11.793° NNE |
| 4 mins | 2025-11-06 17:33:12.091Z | 266.675° W | 2025-11-06 17:34:12.091Z | 279.672° WNW | 14.913° | 2025-11-06 17:37:12.091Z | 317.079° NNW |
| 4 mins | 2025-11-07 02:22:12.091Z | 57.582° ENE | 2025-11-07 02:23:12.091Z | 70.345° E | 14.242° | 2025-11-07 02:26:12.091Z | 106.586° ESE |
| 8 mins | 2025-11-07 04:01:12.091Z | 345.437° N | 2025-11-07 04:04:12.091Z | 296.717° NW | 40.349° | 2025-11-07 04:09:12.091Z | 193.451° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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