IRIDIUM 118, 42807
Orbit data source: Space-Track
IRIDIUM 118, 42807 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 25 Jun 2017 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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42807 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK 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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 118
1 42807U 17039E 25357.21781170 .00000296 00000-0 98454-4 0 9991
2 42807 86.3959 67.1978 0002045 97.9807 262.1621 14.34219177444722Epoch: 2025-12-23T05:13Z
TLE epoch observation values (Epoch: 2025-12-23T05:13:38.930Z)
Latitude
-0.00004°
Longitude
-103.21913°
Altitude
780.913 km
Speed
7.463 km/s
True Right ascension
04h 28m 47s
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
13:43:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.09 km
Perigee altitude
773.164 km
Semi-major axis
7,152.764 km
Eccentricity
0.0002
Inclination
86.3959°
RAAN
67.1978°
Arg. of periapsis
97.9807°
True anomaly
262.13889°
Mean anomaly
262.1621°
Eccentric anomaly
262.15049°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000098454
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Other satellites on launch #39 in the year 2017 (2017-06-25 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 118 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 | 2025-12-23 15:52:03.724Z | 38.294° NE | 2025-12-23 15:55:03.724Z | 78.054° E | 18.115° | 2025-12-23 15:58:03.724Z | 116.679° SE |
| 8 mins | 2025-12-23 17:32:03.724Z | 340.559° N | 2025-12-23 17:36:03.724Z | 267.887° W | 35.824° | 2025-12-23 17:40:03.724Z | 204.167° SW |
| 8 mins | 2025-12-24 04:48:03.724Z | 145.152° SSE | 2025-12-24 04:51:03.724Z | 94.36° ESE | 32.412° | 2025-12-24 04:56:03.724Z | 18.422° NNE |
| 6 mins | 2025-12-24 06:30:03.724Z | 249.844° W | 2025-12-24 06:32:03.724Z | 279.928° WNW | 20.568° | 2025-12-24 06:36:03.724Z | 331.859° 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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