IRIDIUM 168, 43924
Orbit data source: Space-Track
IRIDIUM 168, 43924 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 11 Jan 2019 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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43924 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS 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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 IRIDIUM 168
1 43924U 19002C 25256.84628409 .00000104 00000-0 29923-4 0 9999
2 43924 86.3934 109.2151 0002111 88.2507 271.8930 14.34217865349367Epoch: 2025-09-13T20:18Z
TLE epoch observation values (Epoch: 2025-09-13T20:18:38.945Z)
Latitude
-0.00008°
Longitude
171.47904°
Altitude
780.668 km
Speed
7.464 km/s
True Right ascension
07h 16m 51s
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
02:49:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.141 km
Perigee altitude
773.121 km
Semi-major axis
7,152.768 km
Eccentricity
0.00021
Inclination
86.3934°
RAAN
109.2151°
Arg. of periapsis
88.2507°
True anomaly
271.86882°
Mean anomaly
271.893°
Eccentric anomaly
271.88091°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000029923
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Other satellites on launch #2 in the year 2019 (2019-01-11 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 168 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 | 2025-09-14 14:50:08.341Z | 182.648° SSW | 2025-09-14 14:55:08.341Z | 334.385° NNW | 44.706° | 2025-09-14 14:59:08.341Z | 1.185° NNE |
| 7 mins | 2025-09-15 01:22:08.341Z | 33.824° NE | 2025-09-15 01:25:08.341Z | 76.849° E | 22.051° | 2025-09-15 01:29:08.341Z | 130.012° SE |
| 7 mins | 2025-09-15 03:03:08.341Z | 327.937° NNW | 2025-09-15 03:06:08.341Z | 271.401° WNW | 30.745° | 2025-09-15 03:10:08.341Z | 212.326° SW |
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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