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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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: 14 hours ago
TLE from 14 hours ago
0 IRIDIUM 118
1 42807U 17039E 26305.05984804 .00000055 00000-0 12728-4 0 9999
2 42807 86.3923 296.4264 0002269 89.4274 270.7182 14.34217977489564Epoch: 2026-11-01T01:26Z
TLE epoch observation values (Epoch: 2026-11-01T01:26:10.870Z)
Latitude
-0.00001°
Longitude
-125.47554°
Altitude
780.697 km
Speed
7.464 km/s
True Right ascension
19h 45m 42s
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
11:34:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.254 km
Perigee altitude
773.008 km
Semi-major axis
7,152.768 km
Eccentricity
0.00023
Inclination
86.3923°
RAAN
296.4264°
Arg. of periapsis
89.4274°
True anomaly
270.6922°
Mean anomaly
270.7182°
Eccentric anomaly
270.7052°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000012728
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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 | 2026-11-01 23:19:25.330Z | 141.424° SSE | 2026-11-01 23:23:25.330Z | 84.627° E | 30.894° | 2026-11-01 23:27:25.330Z | 26.861° NE |
| 7 mins | 2026-11-02 01:01:25.330Z | 235.799° WSW | 2026-11-02 01:04:25.330Z | 286.507° WNW | 28.188° | 2026-11-02 01:08:25.330Z | 338.469° N |
| 9 mins | 2026-11-02 11:30:25.330Z | 3.426° NNE | 2026-11-02 11:34:25.330Z | 75.115° E | 72.263° | 2026-11-02 11:39:25.330Z | 171.252° S |
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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