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: 12 hours ago
TLE from 12 hours ago
0 IRIDIUM 168
1 43924U 19002C 25302.89350629 -.00000059 00000-0 -28008-4 0 9996
2 43924 86.3933 89.9452 0002005 90.9590 269.1835 14.34216865355964Epoch: 2025-10-29T21:26Z
TLE epoch observation values (Epoch: 2025-10-29T21:26:38.943Z)
Latitude
-0.00007°
Longitude
89.82282°
Altitude
780.742 km
Speed
7.463 km/s
True Right ascension
05h 59m 46s
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
04:52:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.069 km
Perigee altitude
773.201 km
Semi-major axis
7,152.772 km
Eccentricity
0.0002
Inclination
86.3933°
RAAN
89.9452°
Arg. of periapsis
90.959°
True anomaly
269.16053°
Mean anomaly
269.1835°
Eccentric anomaly
269.17201°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000028008
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-30 09:18:41.522Z | 113.682° SE | 2025-10-30 09:21:41.522Z | 74.642° E | 16.708° | 2025-10-30 09:23:41.522Z | 48.817° ENE |
| 8 mins | 2025-10-30 10:57:41.522Z | 204.696° SW | 2025-10-30 11:01:41.522Z | 279.36° WNW | 37.503° | 2025-10-30 11:05:41.522Z | 347.974° N |
| 8 mins | 2025-10-30 21:28:41.522Z | 21.747° NNE | 2025-10-30 21:31:41.522Z | 72.082° E | 32.357° | 2025-10-30 21:36:41.522Z | 150.842° SSE |
| 6 mins | 2025-10-30 23:09:41.522Z | 317.853° NNW | 2025-10-30 23:12:41.522Z | 274.847° WNW | 20.417° | 2025-10-30 23:15:41.522Z | 235.148° WSW |
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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