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, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 IRIDIUM 160
1 43569U 18061A 25338.47595201 .00000430 00000-0 14646-3 0 9998
2 43569 86.3972 138.2041 0001895 83.3479 276.7932 14.34219858385467Epoch: 2025-12-04T11:25Z
TLE epoch observation values (Epoch: 2025-12-04T11:25:22.253Z)
Latitude
-0.00008°
Longitude
-106.67048°
Altitude
780.551 km
Speed
7.464 km/s
True Right ascension
09h 12m 48s
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
04:44:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.98 km
Perigee altitude
773.269 km
Semi-major axis
7,152.762 km
Eccentricity
0.00019
Inclination
86.3972°
RAAN
138.2041°
Arg. of periapsis
83.3479°
True anomaly
276.77164°
Mean anomaly
276.7932°
Eccentric anomaly
276.78242°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.00014646
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Other satellites on launch #61 in the year 2018 (2018-07-25 UTC)
Did you know?
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 | 2025-12-05 10:58:19.431Z | 163.322° S | 2025-12-05 11:03:19.431Z | 74.678° E | 38.838° | 2025-12-05 11:07:19.431Z | 14.146° NNE |
| 4 mins | 2025-12-05 12:42:19.431Z | 261.106° W | 2025-12-05 12:44:19.431Z | 287.78° WNW | 15.76° | 2025-12-05 12:46:19.431Z | 313.384° NW |
| 8 mins | 2025-12-05 23:10:19.431Z | 348.349° N | 2025-12-05 23:14:19.431Z | 261.986° W | 41.952° | 2025-12-05 23:18:19.431Z | 192.533° SSW |
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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