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, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 118
1 42807U 17039E 25294.98429285 -.00000013 00000-0 -11765-4 0 9990
2 42807 86.3921 93.2206 0002169 91.9754 268.1690 14.34217483435806Epoch: 2025-10-21T23:37Z
TLE epoch observation values (Epoch: 2025-10-21T23:37:22.902Z)
Latitude
-0.00003°
Longitude
68.21076°
Altitude
780.769 km
Speed
7.463 km/s
True Right ascension
06h 12m 52s
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
03:18:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.184 km
Perigee altitude
773.081 km
Semi-major axis
7,152.77 km
Eccentricity
0.00022
Inclination
86.3921°
RAAN
93.2206°
Arg. of periapsis
91.9754°
True anomaly
268.14416°
Mean anomaly
268.169°
Eccentric anomaly
268.15658°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000011765
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-22 11:27:57.075Z | 192.113° SSW | 2025-10-22 11:31:57.075Z | 286.257° WNW | 43.117° | 2025-10-22 11:36:57.075Z | 357.682° N |
| 7 mins | 2025-10-22 21:58:57.075Z | 29.129° NE | 2025-10-22 22:01:57.075Z | 74.946° E | 25.948° | 2025-10-22 22:05:57.075Z | 135.19° SSE |
| 7 mins | 2025-10-22 23:39:57.075Z | 323.624° NNW | 2025-10-22 23:42:57.075Z | 273.696° WNW | 26.339° | 2025-10-22 23:46:57.075Z | 219.071° SW |
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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