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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 IRIDIUM 118
1 42807U 17039E 25257.58836698 .00000042 00000-0 80401-5 0 9999
2 42807 86.3929 108.8717 0001940 91.1177 269.0241 14.34217778430445Epoch: 2025-09-14T14:07Z
TLE epoch observation values (Epoch: 2025-09-14T14:07:14.907Z)
Latitude
-0.00001°
Longitude
-96.74563°
Altitude
780.742 km
Speed
7.463 km/s
True Right ascension
07h 15m 29s
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
02:55:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.019 km
Perigee altitude
773.244 km
Semi-major axis
7,152.769 km
Eccentricity
0.00019
Inclination
86.3929°
RAAN
108.8717°
Arg. of periapsis
91.1177°
True anomaly
269.00187°
Mean anomaly
269.0241°
Eccentric anomaly
269.01299°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000080401
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-15 13:41:48.837Z | 126.612° SE | 2025-09-15 13:44:48.837Z | 86.685° E | 21.137° | 2025-09-15 13:48:48.837Z | 33.235° NE |
| 8 mins | 2025-09-15 15:21:48.837Z | 215.789° SW | 2025-09-15 15:25:48.837Z | 285.171° WNW | 31.546° | 2025-09-15 15:29:48.837Z | 343.346° N |
| 8 mins | 2025-09-16 01:52:48.837Z | 15.911° NNE | 2025-09-16 01:55:48.837Z | 76.759° E | 38.339° | 2025-09-16 02:00:48.837Z | 160.505° S |
| 4 mins | 2025-09-16 03:34:48.837Z | 299.853° NW | 2025-09-16 03:35:48.837Z | 286.393° WNW | 16.019° | 2025-09-16 03:38:48.837Z | 247.915° W |
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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