IRIDIUM 117, 42808
Orbit data source: Space-Track
IRIDIUM 117, 42808 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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42808 intel report (Beta)
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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: 12 hours ago
TLE from 12 hours ago
0 IRIDIUM 117
1 42808U 17039F 26315.68369133 .00000030 00000-0 36117-5 0 9994
2 42808 86.3928 291.9356 0002215 90.0047 270.1402 14.34217695491119Epoch: 2026-11-11T16:24Z
TLE epoch observation values (Epoch: 2026-11-11T16:24:30.930Z)
Latitude
-0.00011°
Longitude
-5.02129°
Altitude
780.715 km
Speed
7.463 km/s
True Right ascension
19h 27m 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
00:45:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.216 km
Perigee altitude
773.048 km
Semi-major axis
7,152.769 km
Eccentricity
0.00022
Inclination
86.3928°
RAAN
291.9356°
Arg. of periapsis
90.0047°
True anomaly
270.11482°
Mean anomaly
270.1402°
Eccentric anomaly
270.12751°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000036117
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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 117 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 | 2026-11-12 09:43:46.878Z | 25.597° NE | 2026-11-12 09:47:46.878Z | 77.199° E | 24.009° | 2026-11-12 09:51:46.878Z | 130.123° SE |
| 7 mins | 2026-11-12 11:25:46.878Z | 327.734° NNW | 2026-11-12 11:28:46.878Z | 270.898° WNW | 36.622° | 2026-11-12 11:32:46.878Z | 212.234° SW |
| 8 mins | 2026-11-12 22:40:46.878Z | 154.305° SSE | 2026-11-12 22:43:46.878Z | 97.815° ESE | 50.205° | 2026-11-12 22:48:46.878Z | 14.074° NNE |
| 5 mins | 2026-11-13 00:22:46.878Z | 253.984° W | 2026-11-13 00:24:46.878Z | 280.244° WNW | 17.642° | 2026-11-13 00:27:46.878Z | 319.243° NNW |
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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