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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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: 20 hours ago
TLE from 20 hours ago
0 IRIDIUM 117
1 42808U 17039F 25304.84067265 .00000143 00000-0 43908-4 0 9990
2 42808 86.3927 89.0561 0001986 86.6644 273.4779 14.34221993437243Epoch: 2025-10-31T20:10Z
TLE epoch observation values (Epoch: 2025-10-31T20:10:34.116Z)
Latitude
-0.00005°
Longitude
106.03462°
Altitude
780.618 km
Speed
7.464 km/s
True Right ascension
05h 56m 13s
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
12:09:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.038 km
Perigee altitude
773.197 km
Semi-major axis
7,152.755 km
Eccentricity
0.0002
Inclination
86.3927°
RAAN
89.0561°
Arg. of periapsis
86.6644°
True anomaly
273.45518°
Mean anomaly
273.4779°
Eccentric anomaly
273.46654°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.000043908
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-01 21:51:24.524Z | 357.639° N | 2025-11-01 21:56:24.524Z | 6.913° NNE | 44.851° | 2025-11-01 22:01:24.524Z | 178.668° S |
| 5 mins | 2025-11-02 09:10:24.524Z | 107.696° ESE | 2025-11-02 09:12:24.524Z | 77.351° E | 19.575° | 2025-11-02 09:15:24.524Z | 38.421° NE |
| 8 mins | 2025-11-02 10:49:24.524Z | 216.553° SW | 2025-11-02 10:52:24.524Z | 272.228° WNW | 33.661° | 2025-11-02 10:57:24.524Z | 347.873° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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