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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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: 2 days ago
TLE from 2 days ago
0 IRIDIUM 160
1 43569U 18061A 26171.40924192 -.00000006 00000-0 -92041-5 0 9990
2 43569 86.3958 55.4502 0002176 85.4709 274.6735 14.34217420413839Epoch: 2026-06-20T09:49Z
TLE epoch observation values (Epoch: 2026-06-20T09:49:18.501Z)
Latitude
-0.00008°
Longitude
-0.50117°
Altitude
780.593 km
Speed
7.464 km/s
True Right ascension
03h 41m 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
21:35:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.189 km
Perigee altitude
773.076 km
Semi-major axis
7,152.77 km
Eccentricity
0.00022
Inclination
86.3958°
RAAN
55.4502°
Arg. of periapsis
85.4709°
True anomaly
274.64865°
Mean anomaly
274.6735°
Eccentric anomaly
274.66107°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000092041
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 15:32:39.404Z | 118.393° SE | 2026-06-22 15:35:39.404Z | 79.935° E | 17.738° | 2026-06-22 15:38:39.404Z | 41.57° NE |
| 8 mins | 2026-06-22 17:12:39.404Z | 210.801° SW | 2026-06-22 17:15:39.404Z | 265.681° W | 35.99° | 2026-06-22 17:20:39.404Z | 349.388° N |
| 8 mins | 2026-06-23 03:42:39.404Z | 17.701° NNE | 2026-06-23 03:46:39.404Z | 91.281° ESE | 33.783° | 2026-06-23 03:50:39.404Z | 151.01° SSE |
| 5 mins | 2026-06-23 05:24:39.404Z | 309.849° NW | 2026-06-23 05:26:39.404Z | 280.868° WNW | 19.446° | 2026-06-23 05:29:39.404Z | 239.907° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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