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: 12 hours ago
TLE from 12 hours ago
0 IRIDIUM 168
1 43924U 19002C 25260.68355242 .00000053 00000-0 11809-4 0 9995
2 43924 86.3925 107.6096 0002145 88.8484 271.2958 14.34217831349912Epoch: 2025-09-17T16:24Z
TLE epoch observation values (Epoch: 2025-09-17T16:24:18.929Z)
Latitude
0.00004°
Longitude
-135.32525°
Altitude
780.683 km
Speed
7.464 km/s
True Right ascension
07h 10m 26s
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
21:12:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.166 km
Perigee altitude
773.097 km
Semi-major axis
7,152.768 km
Eccentricity
0.00021
Inclination
86.3925°
RAAN
107.6096°
Arg. of periapsis
88.8484°
True anomaly
271.27123°
Mean anomaly
271.2958°
Eccentric anomaly
271.28351°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000011809
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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 | 2025-09-18 14:17:18.720Z | 173.254° S | 2025-09-18 14:21:18.720Z | 112.25° ESE | 43.788° | 2025-09-18 14:26:18.720Z | 6.558° NNE |
| 5 mins | 2025-09-19 00:49:18.720Z | 43.901° NE | 2025-09-19 00:51:18.720Z | 70.741° E | 17.872° | 2025-09-19 00:54:18.720Z | 111.678° ESE |
| 8 mins | 2025-09-19 02:29:18.720Z | 337.774° N | 2025-09-19 02:32:18.720Z | 285.241° WNW | 35.758° | 2025-09-19 02:37:18.720Z | 201.726° SSW |
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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