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: 6 hours ago
TLE from 6 hours ago
0 IRIDIUM 160
1 43569U 18061A 26304.10896370 .00000017 00000-0 -10235-5 0 9997
2 43569 86.4000 359.9836 0002130 94.7160 265.4279 14.34217717432857Epoch: 2026-10-31T02:36Z
TLE epoch observation values (Epoch: 2026-10-31T02:36:54.463Z)
Latitude
-0.00004°
Longitude
-78.66274°
Altitude
780.84 km
Speed
7.463 km/s
True Right ascension
23h 59m 56s
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
04:43:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.155 km
Perigee altitude
773.108 km
Semi-major axis
7,152.769 km
Eccentricity
0.00021
Inclination
86.4°
RAAN
359.9836°
Arg. of periapsis
94.716°
True anomaly
265.40357°
Mean anomaly
265.4279°
Eccentric anomaly
265.41574°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000010235
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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 | 2026-10-31 14:55:47.125Z | 37.198° NE | 2026-10-31 14:58:47.125Z | 77.634° E | 20.303° | 2026-10-31 15:01:47.125Z | 117.57° SE |
| 8 mins | 2026-10-31 16:35:47.125Z | 339.353° N | 2026-10-31 16:39:47.125Z | 269.315° W | 43.733° | 2026-10-31 16:43:47.125Z | 206.321° SW |
| 8 mins | 2026-11-01 03:51:47.125Z | 147.149° SSE | 2026-11-01 03:54:47.125Z | 94.512° ESE | 41.985° | 2026-11-01 03:59:47.125Z | 17.305° NNE |
| 6 mins | 2026-11-01 05:33:47.125Z | 251.186° W | 2026-11-01 05:35:47.125Z | 280.272° WNW | 20.951° | 2026-11-01 05:39:47.125Z | 331.039° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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