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, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 IRIDIUM 168
1 43924U 19002C 25303.94003300 .00001150 00000-0 40357-3 0 9995
2 43924 86.3933 89.5071 0002090 89.8324 270.3111 14.34219408356118Epoch: 2025-10-30T22:33Z
TLE epoch observation values (Epoch: 2025-10-30T22:33:38.851Z)
Latitude
-0.00004°
Longitude
71.6036°
Altitude
780.705 km
Speed
7.463 km/s
True Right ascension
05h 58m 01s
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
03:52:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.121 km
Perigee altitude
773.131 km
Semi-major axis
7,152.763 km
Eccentricity
0.00021
Inclination
86.3933°
RAAN
89.5071°
Arg. of periapsis
89.8324°
True anomaly
270.28715°
Mean anomaly
270.3111°
Eccentric anomaly
270.29913°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00040357
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-31 10:22:55.397Z | 179.599° S | 2025-10-31 10:27:55.397Z | 142.717° SSE | 44.891° | 2025-10-31 10:32:55.397Z | 3.3° NNE |
| 6 mins | 2025-10-31 20:55:55.397Z | 42.343° NE | 2025-10-31 20:57:55.397Z | 71.237° E | 20.404° | 2025-10-31 21:01:55.397Z | 125.197° SE |
| 8 mins | 2025-10-31 22:35:55.397Z | 333.102° NNW | 2025-10-31 22:38:55.397Z | 281.023° WNW | 32.531° | 2025-10-31 22:43:55.397Z | 206.381° 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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