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: 8 hours ago
TLE from 8 hours ago
0 IRIDIUM 118
1 42807U 17039E 25312.77526447 .00000167 00000-0 52744-4 0 9996
2 42807 86.3944 85.7776 0002228 89.8298 270.3154 14.34218899438359Epoch: 2025-11-08T18:36Z
TLE epoch observation values (Epoch: 2025-11-08T18:36:22.850Z)
Latitude
0.00008°
Longitude
118.48236°
Altitude
780.706 km
Speed
7.463 km/s
True Right ascension
05h 43m 06s
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
22:22:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.222 km
Perigee altitude
773.034 km
Semi-major axis
7,152.765 km
Eccentricity
0.00022
Inclination
86.3944°
RAAN
85.7776°
Arg. of periapsis
89.8298°
True anomaly
270.28987°
Mean anomaly
270.3154°
Eccentric anomaly
270.30263°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000052744
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-09 09:48:24.964Z | 194.327° SSW | 2025-11-09 09:51:24.964Z | 247.569° W | 42.574° | 2025-11-09 09:56:24.964Z | 356.569° N |
| 7 mins | 2025-11-09 20:19:24.964Z | 34.175° NE | 2025-11-09 20:22:24.964Z | 86.298° E | 26.177° | 2025-11-09 20:26:24.964Z | 139.298° SSE |
| 7 mins | 2025-11-09 21:59:24.964Z | 327.614° NNW | 2025-11-09 22:02:24.964Z | 283.603° WNW | 25.922° | 2025-11-09 22:06:24.964Z | 222.701° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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