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: 1 day ago
TLE from 1 day ago
0 IRIDIUM 118
1 42807U 17039E 26262.08244138 .00000107 00000-0 31297-4 0 9993
2 42807 86.3975 314.4077 0002248 94.9692 265.1760 14.34218072483400Epoch: 2026-09-19T01:58Z
TLE epoch observation values (Epoch: 2026-09-19T01:58:42.935Z)
Latitude
-0.00005°
Longitude
-73.26728°
Altitude
780.853 km
Speed
7.463 km/s
True Right ascension
20h 57m 37s
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
19:05:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.239 km
Perigee altitude
773.023 km
Semi-major axis
7,152.768 km
Eccentricity
0.00022
Inclination
86.3975°
RAAN
314.4077°
Arg. of periapsis
94.9692°
True anomaly
265.15033°
Mean anomaly
265.176°
Eccentric anomaly
265.16317°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000031297
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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 | 2026-09-20 03:12:47.638Z | 137.668° SSE | 2026-09-20 03:16:47.638Z | 86.106° E | 26.542° | 2026-09-20 03:20:47.638Z | 30.268° NE |
| 7 mins | 2026-09-20 04:54:47.638Z | 230.162° WSW | 2026-09-20 04:57:47.638Z | 285.549° WNW | 32.743° | 2026-09-20 05:01:47.638Z | 340.693° N |
| 8 mins | 2026-09-20 15:24:47.638Z | 11.137° NNE | 2026-09-20 15:27:47.638Z | 74.436° E | 61.254° | 2026-09-20 15:32:47.638Z | 165.675° S |
| 4 mins | 2026-09-20 17:06:47.638Z | 298.386° NW | 2026-09-20 17:07:47.638Z | 285.816° WNW | 14.419° | 2026-09-20 17:10:47.638Z | 250.267° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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