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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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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 168
1 43924U 19002C 26090.33771778 .00000182 00000-0 57796-4 0 9993
2 43924 86.4011 26.1957 0002091 85.0176 275.1259 14.34219125377812Epoch: 2026-03-31T08:06Z
TLE epoch observation values (Epoch: 2026-03-31T08:06:18.816Z)
Latitude
0.00005°
Longitude
75.90096°
Altitude
780.58 km
Speed
7.464 km/s
True Right ascension
01h 44m 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
23:05:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.123 km
Perigee altitude
773.131 km
Semi-major axis
7,152.764 km
Eccentricity
0.00021
Inclination
86.4011°
RAAN
26.1957°
Arg. of periapsis
85.0176°
True anomaly
275.10203°
Mean anomaly
275.1259°
Eccentric anomaly
275.11397°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000057796
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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 | 2026-03-31 19:56:36.099Z | 164.436° S | 2026-03-31 20:00:36.099Z | 94.597° ESE | 40.649° | 2026-03-31 20:05:36.099Z | 10.789° NNE |
| 4 mins | 2026-03-31 21:40:36.099Z | 269.25° W | 2026-03-31 21:41:36.099Z | 282.233° WNW | 14.589° | 2026-03-31 21:44:36.099Z | 318.601° NNW |
| 4 mins | 2026-04-01 06:29:36.099Z | 59.676° ENE | 2026-04-01 06:30:36.099Z | 72.765° E | 14.685° | 2026-04-01 06:33:36.099Z | 108.854° ESE |
| 8 mins | 2026-04-01 08:08:36.099Z | 343.72° N | 2026-04-01 08:11:36.099Z | 286.005° WNW | 40.347° | 2026-04-01 08:16:36.099Z | 193.983° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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