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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 160
1 43569U 18061A 25259.49799111 .00000054 00000-0 12136-4 0 9993
2 43569 86.4048 171.1740 0001971 86.3781 273.7641 14.34217834374147Epoch: 2025-09-16T11:57Z
TLE epoch observation values (Epoch: 2025-09-16T11:57:06.431Z)
Latitude
0.00003°
Longitude
-3.79023°
Altitude
780.626 km
Speed
7.464 km/s
True Right ascension
11h 24m 41s
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
14:02:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.041 km
Perigee altitude
773.221 km
Semi-major axis
7,152.768 km
Eccentricity
0.0002
Inclination
86.4048°
RAAN
171.174°
Arg. of periapsis
86.3781°
True anomaly
273.74156°
Mean anomaly
273.7641°
Eccentric anomaly
273.75283°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000012136
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-17 05:17:06.877Z | 33.684° NE | 2025-09-17 05:20:06.877Z | 73.473° E | 20.109° | 2025-09-17 05:24:06.877Z | 125.729° SE |
| 7 mins | 2025-09-17 06:58:06.877Z | 332.677° NNW | 2025-09-17 07:01:06.877Z | 277.32° WNW | 33.129° | 2025-09-17 07:05:06.877Z | 209.962° SW |
| 8 mins | 2025-09-17 18:13:06.877Z | 151.752° SSE | 2025-09-17 18:17:06.877Z | 71.302° E | 34.821° | 2025-09-17 18:21:06.877Z | 17.176° NNE |
| 6 mins | 2025-09-17 19:55:06.877Z | 249.011° W | 2025-09-17 19:57:06.877Z | 275.807° WNW | 18.297° | 2025-09-17 20:01:06.877Z | 327.634° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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