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: 8 hours ago
TLE from 8 hours ago
0 IRIDIUM 160
1 43569U 18061A 26142.73438038 .00000083 00000-0 22537-4 0 9998
2 43569 86.3967 67.4372 0002250 87.5233 272.6221 14.34217497409720Epoch: 2026-05-22T17:37Z
TLE epoch observation values (Epoch: 2026-05-22T17:37:30.464Z)
Latitude
0.00002°
Longitude
-77.30071°
Altitude
780.646 km
Speed
7.464 km/s
True Right ascension
04h 29m 44s
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
11:02:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.242 km
Perigee altitude
773.023 km
Semi-major axis
7,152.769 km
Eccentricity
0.00023
Inclination
86.3967°
RAAN
67.4372°
Arg. of periapsis
87.5233°
True anomaly
272.59634°
Mean anomaly
272.6221°
Eccentric anomaly
272.60922°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000022537
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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 | 2026-05-23 05:56:10.865Z | 37.222° NE | 2026-05-23 05:59:10.865Z | 75.035° E | 17.161° | 2026-05-23 06:02:10.865Z | 113.519° SE |
| 8 mins | 2026-05-23 07:37:10.865Z | 337.415° NNW | 2026-05-23 07:40:10.865Z | 275.366° WNW | 37.204° | 2026-05-23 07:45:10.865Z | 199.068° SSW |
| 8 mins | 2026-05-23 18:52:10.865Z | 144.496° SSE | 2026-05-23 18:56:10.865Z | 72.269° E | 30.766° | 2026-05-23 19:00:10.865Z | 20.477° NNE |
| 6 mins | 2026-05-23 20:34:10.865Z | 246.069° WSW | 2026-05-23 20:36:10.865Z | 276.277° WNW | 21.544° | 2026-05-23 20:40:10.865Z | 331.223° 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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