IRIDIUM 160, 43569
Orbit data source: Space-Track
IRIDIUM 160, 43569 is a payload satellite owned by Iridium (US) in LEO that was launched on Wed, 25 Jul 2018 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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43569 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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 IRIDIUM 160
1 43569U 18061A 25258.73053741 .00000114 00000-0 33616-4 0 9994
2 43569 86.4049 171.4940 0001974 85.9783 274.1639 14.34217902374039Epoch: 2025-09-15T17:31Z
TLE epoch observation values (Epoch: 2025-09-15T17:31:58.432Z)
Latitude
0.00005°
Longitude
-86.43046°
Altitude
780.615 km
Speed
7.464 km/s
True Right ascension
11h 25m 58s
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
02:15:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.043 km
Perigee altitude
773.219 km
Semi-major axis
7,152.768 km
Eccentricity
0.0002
Inclination
86.4049°
RAAN
171.494°
Arg. of periapsis
85.9783°
True anomaly
274.14134°
Mean anomaly
274.1639°
Eccentric anomaly
274.15262°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000033616
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Other satellites on launch #61 in the year 2018 (2018-07-25 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 160 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 | 2025-09-16 18:45:51.279Z | 178.634° S | 2025-09-16 18:49:51.279Z | 150.417° SSE | 44.616° | 2025-09-16 18:54:51.279Z | 3.738° NNE |
| 6 mins | 2025-09-17 05:17:51.279Z | 41.241° NE | 2025-09-17 05:20:51.279Z | 85.688° E | 19.929° | 2025-09-17 05:23:51.279Z | 123.572° SE |
| 8 mins | 2025-09-17 06:57:51.279Z | 334.665° NNW | 2025-09-17 07:00:51.279Z | 285.051° WNW | 32.84° | 2025-09-17 07:05:51.279Z | 206.246° SW |
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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