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: 18 hours ago
TLE from 18 hours ago
0 IRIDIUM 160
1 43569U 18061A 25308.54525889 -.00000008 00000-0 -98160-5 0 9996
2 43569 86.3983 150.7079 0002235 88.9061 271.2391 14.34217867381177Epoch: 2025-11-04T13:05Z
TLE epoch observation values (Epoch: 2025-11-04T13:05:10.368Z)
Latitude
0.00001°
Longitude
-89.61604°
Altitude
780.683 km
Speed
7.464 km/s
True Right ascension
10h 02m 49s
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
03:29:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.23 km
Perigee altitude
773.033 km
Semi-major axis
7,152.768 km
Eccentricity
0.00022
Inclination
86.3983°
RAAN
150.7079°
Arg. of periapsis
88.9061°
True anomaly
271.21349°
Mean anomaly
271.2391°
Eccentric anomaly
271.2263°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000009816
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-05 14:20:04.466Z | 191.985° SSW | 2025-11-05 14:23:04.466Z | 248.038° W | 43.418° | 2025-11-05 14:28:04.466Z | 357.827° N |
| 7 mins | 2025-11-06 00:51:04.466Z | 36.109° NE | 2025-11-06 00:54:04.466Z | 87.399° E | 25.042° | 2025-11-06 00:58:04.466Z | 138.235° SSE |
| 7 mins | 2025-11-06 02:31:04.466Z | 328.151° NNW | 2025-11-06 02:34:04.466Z | 282.445° WNW | 27.054° | 2025-11-06 02:38:04.466Z | 220.612° 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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