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: 14 hours ago
TLE from 14 hours ago
0 IRIDIUM 160
1 43569U 18061A 25311.96391867 -.00000100 00000-0 -42938-4 0 9997
2 43569 86.3981 149.2803 0002213 87.9423 272.2026 14.34216446381662Epoch: 2025-11-07T23:08Z
TLE epoch observation values (Epoch: 2025-11-07T23:08:02.573Z)
Latitude
-0.00002°
Longitude
114.86924°
Altitude
780.662 km
Speed
7.464 km/s
True Right ascension
09h 57m 07s
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
09:04:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.219 km
Perigee altitude
773.053 km
Semi-major axis
7,152.773 km
Eccentricity
0.00022
Inclination
86.3981°
RAAN
149.2803°
Arg. of periapsis
87.9423°
True anomaly
272.17726°
Mean anomaly
272.2026°
Eccentric anomaly
272.18993°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000042938
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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 | 2025-11-08 14:18:30.817Z | 201.009° SSW | 2025-11-08 14:23:30.817Z | 277.689° WNW | 37.199° | 2025-11-08 14:27:30.817Z | 347.427° N |
| 8 mins | 2025-11-09 00:50:30.817Z | 21.088° NNE | 2025-11-09 00:53:30.817Z | 70.77° E | 32.59° | 2025-11-09 00:58:30.817Z | 151.113° SSE |
| 6 mins | 2025-11-09 02:31:30.817Z | 318.021° NNW | 2025-11-09 02:34:30.817Z | 275.536° WNW | 20.186° | 2025-11-09 02:37:30.817Z | 235.833° WSW |
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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