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: 11 hours ago
TLE from 11 hours ago
0 IRIDIUM 160
1 43569U 18061A 26123.89687945 .00000229 00000-0 74611-4 0 9999
2 43569 86.3951 75.3123 0002176 86.7468 273.3977 14.34218170407029Epoch: 2026-05-03T21:31Z
TLE epoch observation values (Epoch: 2026-05-03T21:31:30.384Z)
Latitude
0°
Longitude
-109.35814°
Altitude
780.625 km
Speed
7.464 km/s
True Right ascension
05h 01m 14s
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
16:01:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.187 km
Perigee altitude
773.074 km
Semi-major axis
7,152.767 km
Eccentricity
0.00022
Inclination
86.3951°
RAAN
75.3123°
Arg. of periapsis
86.7468°
True anomaly
273.37281°
Mean anomaly
273.3977°
Eccentric anomaly
273.38525°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000074611
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-04 08:13:12.947Z | 83.693° E | 2026-05-04 08:13:12.947Z | 83.693° E | 27.884° | 2026-05-04 08:17:12.947Z | 140.754° SSE |
| 6 mins | 2026-05-04 09:51:12.947Z | 317.35° NNW | 2026-05-04 09:53:12.947Z | 285.764° WNW | 24.269° | 2026-05-04 09:57:12.947Z | 225.97° WSW |
| 9 mins | 2026-05-04 21:05:12.947Z | 170.151° S | 2026-05-04 21:09:12.947Z | 84.935° E | 43.158° | 2026-05-04 21:14:12.947Z | 7.578° NNE |
| 5 mins | 2026-05-05 07:37:12.947Z | 47.661° ENE | 2026-05-05 07:39:12.947Z | 74.626° E | 16.958° | 2026-05-05 07:42:12.947Z | 112.985° SE |
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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