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: 22 hours ago
TLE from 22 hours ago
0 IRIDIUM 117
1 42808U 17039F 26307.45100548 -.00000001 00000-0 -72485-5 0 9991
2 42808 86.3919 295.3817 0002066 90.9185 269.2247 14.34217315489937Epoch: 2026-11-03T10:49Z
TLE epoch observation values (Epoch: 2026-11-03T10:49:26.873Z)
Latitude
-0.00007°
Longitude
90.30624°
Altitude
780.74 km
Speed
7.463 km/s
True Right ascension
19h 41m 31s
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
04:17:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.111 km
Perigee altitude
773.155 km
Semi-major axis
7,152.77 km
Eccentricity
0.00021
Inclination
86.3919°
RAAN
295.3817°
Arg. of periapsis
90.9185°
True anomaly
269.20103°
Mean anomaly
269.2247°
Eccentric anomaly
269.21286°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000072485
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-11-04 10:50:25.785Z | 15.782° NNE | 2026-11-04 10:54:25.785Z | 70.41° E | 37.653° | 2026-11-04 10:59:25.785Z | 149.107° SSE |
| 6 mins | 2026-11-04 12:32:25.785Z | 319.336° NNW | 2026-11-04 12:35:25.785Z | 276.121° WNW | 22.929° | 2026-11-04 12:38:25.785Z | 234.916° WSW |
| 8 mins | 2026-11-04 23:47:25.785Z | 177.233° S | 2026-11-04 23:50:25.785Z | 153.955° SSE | 75.967° | 2026-11-04 23:55:25.785Z | 4.242° NNE |
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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