IRIDIUM 180, 43922
Orbit data source: Space-Track
IRIDIUM 180, 43922 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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43922 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: 1 day ago
TLE from 1 day ago
0 IRIDIUM 180
1 43922U 19002A 25286.50424644 .00000010 00000-0 -35513-5 0 9998
2 43922 86.3915 96.7327 0002112 90.9755 269.1682 14.34217524353636Epoch: 2025-10-13T12:06Z
TLE epoch observation values (Epoch: 2025-10-13T12:06:06.892Z)
Latitude
-0.0001°
Longitude
-107.1021°
Altitude
780.741 km
Speed
7.463 km/s
True Right ascension
06h 26m 55s
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
10:49:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.143 km
Perigee altitude
773.122 km
Semi-major axis
7,152.77 km
Eccentricity
0.00021
Inclination
86.3915°
RAAN
96.7327°
Arg. of periapsis
90.9755°
True anomaly
269.144°
Mean anomaly
269.1682°
Eccentric anomaly
269.1561°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000035513
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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 180 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 | 2025-10-14 22:11:20.695Z | 44.874° NE | 2025-10-14 22:13:20.695Z | 68.586° E | 13.986° | 2025-10-14 22:16:20.695Z | 105.001° ESE |
| 8 mins | 2025-10-14 23:51:20.695Z | 346.38° N | 2025-10-14 23:55:20.695Z | 247.459° WSW | 40.749° | 2025-10-14 23:59:20.695Z | 193.274° SSW |
| 7 mins | 2025-10-15 11:07:20.695Z | 133.525° SE | 2025-10-15 11:10:20.695Z | 85.363° E | 26.806° | 2025-10-15 11:14:20.695Z | 27.317° NE |
| 7 mins | 2025-10-15 12:48:20.695Z | 235.011° WSW | 2025-10-15 12:51:20.695Z | 285.895° WNW | 25.48° | 2025-10-15 12:55:20.695Z | 338.532° N |
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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