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: 6 hours ago
TLE from 6 hours ago
0 IRIDIUM 168
1 43924U 19002C 25365.12702481 .00000109 00000-0 31726-4 0 9993
2 43924 86.3953 63.9257 0002208 97.6173 262.5273 14.34218087364889Epoch: 2025-12-31T03:02Z
TLE epoch observation values (Epoch: 2025-12-31T03:02:54.943Z)
Latitude
-0.00009°
Longitude
-81.60365°
Altitude
780.923 km
Speed
7.463 km/s
True Right ascension
04h 15m 42s
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
08:14:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.21 km
Perigee altitude
773.051 km
Semi-major axis
7,152.768 km
Eccentricity
0.00022
Inclination
86.3953°
RAAN
63.9257°
Arg. of periapsis
97.6173°
True anomaly
262.50221°
Mean anomaly
262.5273°
Eccentric anomaly
262.51476°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000031726
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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 | 2025-12-31 15:20:56.542Z | 25.502° NE | 2025-12-31 15:24:56.542Z | 80.475° E | 23.539° | 2025-12-31 15:28:56.542Z | 133.58° SE |
| 7 mins | 2025-12-31 17:02:56.542Z | 323.865° NNW | 2025-12-31 17:05:56.542Z | 266.973° W | 28.8° | 2025-12-31 17:09:56.542Z | 213.723° SW |
| 8 mins | 2026-01-01 04:17:56.542Z | 157.092° SSE | 2026-01-01 04:20:56.542Z | 93.281° ESE | 39.336° | 2026-01-01 04:25:56.542Z | 12.099° NNE |
| 4 mins | 2026-01-01 06:00:56.542Z | 268.763° W | 2026-01-01 06:01:56.542Z | 282.254° WNW | 15.584° | 2026-01-01 06:04:56.542Z | 319.532° NNW |
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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