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: 8 hours ago
TLE from 8 hours ago
0 IRIDIUM 168
1 43924U 19002C 26125.43128387 .00000177 00000-0 56191-4 0 9997
2 43924 86.4009 11.5439 0002201 85.2863 274.8584 14.34217674382843Epoch: 2026-05-05T10:21Z
TLE epoch observation values (Epoch: 2026-05-05T10:21:02.926Z)
Latitude
-0.00003°
Longitude
-7.02452°
Altitude
780.585 km
Speed
7.464 km/s
True Right ascension
00h 46m 10s
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
02:37:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.206 km
Perigee altitude
773.057 km
Semi-major axis
7,152.769 km
Eccentricity
0.00022
Inclination
86.4009°
RAAN
11.5439°
Arg. of periapsis
85.2863°
True anomaly
274.83327°
Mean anomaly
274.8584°
Eccentric anomaly
274.84583°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000056191
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-06 03:40:03.421Z | 20.99° NNE | 2026-05-06 03:44:03.421Z | 71.89° E | 25.113° | 2026-05-06 03:48:03.421Z | 132.912° SE |
| 7 mins | 2026-05-06 05:22:03.421Z | 325.943° NNW | 2026-05-06 05:25:03.421Z | 277.122° WNW | 27.102° | 2026-05-06 05:29:03.421Z | 219.063° SW |
| 8 mins | 2026-05-06 16:37:03.421Z | 163.353° S | 2026-05-06 16:41:03.421Z | 62.003° ENE | 40.282° | 2026-05-06 16:45:03.421Z | 11.24° NNE |
| 4 mins | 2026-05-06 18:20:03.421Z | 264.485° W | 2026-05-06 18:22:03.421Z | 289.979° WNW | 14.204° | 2026-05-06 18:24:03.421Z | 314.095° NW |
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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