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: 1 day ago
TLE from 1 day ago
0 IRIDIUM 160
1 43569U 18061A 25260.89336172 -.00000021 00000-0 -14394-4 0 9997
2 43569 86.4049 170.5921 0001866 86.5906 273.5503 14.34217468374346Epoch: 2025-09-17T21:26Z
TLE epoch observation values (Epoch: 2025-09-17T21:26:26.452Z)
Latitude
-0.00005°
Longitude
-148.0809°
Altitude
780.637 km
Speed
7.464 km/s
True Right ascension
11h 22m 22s
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
14:27:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.967 km
Perigee altitude
773.298 km
Semi-major axis
7,152.769 km
Eccentricity
0.00019
Inclination
86.4049°
RAAN
170.5921°
Arg. of periapsis
86.5906°
True anomaly
273.52896°
Mean anomaly
273.5503°
Eccentric anomaly
273.53963°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000014394
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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 | 2025-09-19 05:49:38.659Z | 7.344° NNE | 2025-09-19 05:54:38.659Z | 103.91° ESE | 39.505° | 2025-09-19 05:58:38.659Z | 161.821° S |
| 4 mins | 2025-09-19 07:32:38.659Z | 304.363° NW | 2025-09-19 07:34:38.659Z | 278.537° WNW | 14.957° | 2025-09-19 07:36:38.659Z | 253.708° W |
| 8 mins | 2025-09-19 18:46:38.659Z | 195.221° SSW | 2025-09-19 18:50:38.659Z | 303.76° NW | 41.708° | 2025-09-19 18:54:38.659Z | 355.202° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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